ASME SEC II D-M SB PT 3

Subpart 3CHARTS AND TABLES FOR

DETERMINING SHELLTHICKNESS OF COMPONENTSUNDER EXTERNAL PRESSURE

705

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Fig. G 2004 SECTION II

706



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PART D — PROPERTIES (METRIC) Fig. G

FIG

.G

GE

OM

ET

RIC

CH

AR

TF

OR

CO

MP

ON

EN

TS

UN

DE

RE

XT

ER

NA

LO

RC

OM

PR

ES

SIV

EL

OA

DIN

GS

(for

All

Mat

eria

ls)

707



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Fig. CS-1 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

100

9080

70

60

50

40

30

2018

16

14

12

25

35

0.00001

GENERAL NOTE: See Table CS-1 for tabular values.

E � 199.9 � 103

E � 186.2 � 103

E � 168.9 � 103

E � 157.2 � 103

E � 143.4 � 103

260�C

370�C

425�C480�C

Up to 150�C

FIG. CS-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF CARBON OR LOW ALLOY STEELS (Specified Minimum Yield Strength 165 MPa to, but Not

Including, 205 MPa) [Note (1)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

160

140

120

80

90

100

70

60

50

40

30

2018

16

35

25

0.00001


E � 199.9 � 103

E � 186.2 � 103

E � 168.9 � 103

E � 157.2 � 103

E � 143.4 � 103

260�C

370�C

425�C

480�C

Up to 150�C

FIG. CS-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF CARBON OR LOW ALLOY STEELS (Specified Minimum Yield Strength 205 MPa and OverExcept for Materials Within This Range Where Other Specific Charts Are Referenced) AND TYPE 405 AND TYPE 410

STAINLESS STEELS [Note (1)]

708



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PART D — PROPERTIES (METRIC) Fig. CS-4

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

300

250

200

30

35

40

50

60

70

80

90100

120

140

160

180

0.00001

GENERAL NOTES:(a) See Table CS-3 for tabular values.(b) These curves shall not be used for design temperature above 150�C. Above 150�C, use the appropriate temperature curve shown in Fig. CS-2.

E � 200 � 103 Sy � Above 262 to 276, incl.

Sy � 414 and aboveSy � 379

Sy � 345Sy � 310

FIG. CS-3 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF CARBON STEEL, LOW ALLOY STEELS, OR STEELS WITH PROPERTIES ENHANCED BY

HEAT TREATMENT (Specified Minimum Yield Strength Over 262 MPa for Materials Where Other Specific Charts AreNot Referenced) [Notes (1), (2), and (3)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

350

250

300

200180

160

140

120

10090

80

70

60

50

40

35

0.00001


E � 206.8 � 103

E � 198.6 � 103

Class 2 (40�C)

Class 1 (40�C)

Class 2 (150�C)

Class 1 (150�C)

FIG. CS-4 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SA-537 [Note (1)]

709



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Fig. CS-5 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

250

180200

1009080

70

60

50

40

30

35

25

120

140

160

20

0.00001


E � 208.2 � 103 (40�C)E � 206.2 � 103 (95�C)E � 204.1 � 103 (150�C)E � 199.3 � 103 (205�C)

E � 192.4 � 103 (290�C) E � 188.2 � 103 (340�C)

Up to 40�C 95�C 150�C

340�C290�C205�C

FIG. CS-5 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SA-508 CLASS 1 GRADES 2 AND 3; SA-508 CLASS 2 GRADE 2; SA-533 CLASS 1

GRADES A, B, C, AND D; SA-533 CLASS 2 GRADES A, B, C, AND D; OR SA-541 GRADES 2 AND 3

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

1009080

70

60

50

40

35

25

30

12

14

16

18

20

0.00001


E � 206.8 � 103

E � 194.4 � 103

Up to 40�C

95�C150�C

205�C

FIG. CS-6 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SA-562 OR SA-620 CARBON STEEL

710



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PART D — PROPERTIES (METRIC) Fig. HT-2

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

400

350

300

35

40

50

60

70

8090100

120

140

160

180200

250

0.00001

GENERAL NOTE: See Table HT-1 for tabular values.

E � 199.9 � 103

E � 190.3 � 103

E � 173.1 � 103

Up to 95�C

345�C

205�C

FIG. HT-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF QUENCHED AND TEMPERED LOW ALLOY STEEL, SA-517 ALL GRADES, AND SA-592

GRADES A, E, AND F WHERE t ≤ 63.5 mm [Note (1)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

400

350

300

35

40

50

60

70

8090100

120

140

160

180200

250

0.00001

GENERAL NOTES:(a) See Table HT-2 for tabular values.(b) For temperatures over 40�C, use Fig. CS-2.

E � 204.7 � 103

40�C

FIG. HT-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SA-508 GRADE 4N, CLASS 2 OR SA-543 TYPES B AND C, CLASS 2

711



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Fig. HA-1 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

12

14

16

18

20

25

30

35

40

50

60

70

80

90100

0.00001

GENERAL NOTE: See Table HA-1 for tabular values.Up to 40�C

205�C

370�C

480�C

650�C

E � 193.1 � 103

E � 178.6 � 103

E � 164.1 � 103

E � 154.4 � 103

E � 140.0 � 103

FIG. HA-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF AUSTENITIC STEEL (18Cr–8Ni, Type 304) [Note (1)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

160140

120

10090

80

70

60

50

40

30

20

18

35

25

16

0.00001

GENERAL NOTE: See Table HA-2 for tabular values.

Up to 40�C

480�C

650�C

E � 193.1 � 103

E � 178.6 � 103

E � 164.1 � 103

E � 154.4 � 103

E � 140.0 � 103

370�C205�C

FIG. HA-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF AUSTENITIC STEEL [16Cr–12Ni–2Mo, Type 316; 18Cr–10Ni–Ti, Type 321; 18Cr–10Ni–Cb,

Type 347; 25Cr–12Ni, Type 309 (Through 595°C Only); 25Cr–20Ni, Type 310; and 17Cr, Type 430B Stainless Steel(Through 370°C Only)] [Note (1)]

712



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PART D — PROPERTIES (METRIC) Fig. HA-4

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

10090

80

70

60

50

40

30

20

18

16

14

25

35

12

0.00001

GENERAL NOTE: See Table HA-3 for tabular values. Up to 40�C

425�C

E � 193.1 � 103

E � 178.6 � 103

E � 168.9 � 103

E � 159.3 � 103

315�C

205�C

FIG. HA-3 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF AUSTENITIC STEEL (18Cr–8Ni–0.035 Maximum Carbon, Type 304L) [Note (1)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

10090

80

70

60

50

40

30

20

18

16

14

25

35

12

0.00001

GENERAL NOTE: See Table HA-4 for tabular values. Up to 40�C

425�C

E � 193.1 � 103

E � 182.0 � 103

E � 168.9 � 103

E � 159.3 � 103

315�C

205�C

150�C

FIG. HA-4 CHART FOR DETERMINING SHELL THICKNESS OFCOMPONENTS UNDER EXTERNAL PRESSURE WHEN CONSTRUCTED OF AUSTENITIC STEEL

(18Cr–8Ni–Mo–0.035 Maximum Carbon, Types 316L and 317L) [Note (1)]

713



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

250

200

14

161820

25

30

35

50

60

8090100

120

140160180

70

40

0.00001

GENERAL NOTE: See Table HA-5 for tabular values. Room temp.

E � 195 � 103

E � 183 � 103

E � 172 � 103

350�C

205�C

FIG. HA-5 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF Cr–Ni–Mo Alloy S31500

FIG. HA-6 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF 21Cr–11Ni–N Alloy S30815 [Note (4)]

714



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PART D — PROPERTIES (METRIC) Fig. HA-7

0.00001 0.00012 9876543

0.001

Factor A

Fact

or

B

2 98765430.01

2 98765430.1

7

14

21

28

35

4249566370

140

210

280

350

420490560630700

2 9876543

Up to 20�C150�C

E = 201.3 × 103

E = 192.4 × 103


FIG. HA-7 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SA-564 TYPE 630 H1150

715



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700

210

280

140

70

4235

28

21

14

72 3 4 5 6 7 8 9

0.12 3 4 5 6 7 8 9

0.01

Factor A

Fact

or

B

2 3 4 5 6 7 8 90.0010.0001

Up to 20�C100�C400�C

E � 195.1 � 103

E � 189.6 � 103

E � 168.9 � 103


FIG. HA-8 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF DUPLEX STAINLESS STEEL 25Cr–7Ni–3Mo–2W–0.28N (UNS S39274)

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

160140

120

10090

80

70

60

50

40

30

20

18

35

25

16

0.00001

GENERAL NOTE: See Table CI-1 for tabular values.Class 60, up to 345�C

Class 50, up to 345�C



Class 20, up to 345�C E � 151.7 � 103

E � 137.9 � 103

E � 120.7 � 103

E � 100.0 � 103

E � 82.7 � 103

FIG. CI-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF CAST IRON [Note (5)]

716



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PART D — PROPERTIES (METRIC) Fig. NFA-1

FIG. CD-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF CAST DUCTILE IRON WITH A SPECIFIED MINIMUM YIELD STRENGTH OF 275 MPa

[Note (6)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

25

2018

16

14

12

109.0

8.0

7.0

6.0

5.0

4.0

3.0

3.5

2.5

0.00001

GENERAL NOTE: See Table NFA-1 for tabular values. Up to 40�C

205�C

E � 69.0 � 103

E � 66.2 � 103

E � 62.7 � 103

E � 57.2 � 103

150�C

95�C

FIG. NFA-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 3003 IN O AND H112 TEMPERS [Notes (7) and (8)]

717



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Fig. NFA-2 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

80

0.8

0.91.0

1.2

1.4

1.6

1.82.0

3.0

4.0

5.0

6.0

7.0

8.0

9.010

12

14

161820

30

40

50

60

70

35

25

3.5

2.5

0.00001

Up to 40�C

205�C

E � 69.0 � 103

E � 66.2 � 103

E � 62.7 � 103

E � 57.2 � 103

150�C

95�C

GENERAL NOTES:(a) See Table NFA-2 for tabular values.(b) This chart is not to be used for welded construction.

FIG. NFA-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 3003 IN H14 TEMPER [Notes (7) and (8)]

718



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

35

25

201816

14

12

109.0

8.0

7.0

6.0

5.0

4.0

30

3.0

3.5

0.00001

GENERAL NOTE: See Table NFA-3 for tabular values.

Up to 40�C

150�C

205�C

100�C

E � 69.0 � 103

E � 66.2 � 103

E � 62.7 � 103

E � 57.2 � 103

FIG. NFA-3 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 3004 IN O AND H112 TEMPERS [Note (7)]

719



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

100

0.91.0

1.2

1.4

1.6

1.82.0

3.0

4.0

5.0

6.0

7.0

8.09.010

12

14

161820

30

40

50

60

70

8090

35

25

3.5

2.5

0.00001

Up to 40�C

205�C

E � 69.0 � 103

E � 66.2 � 103

E � 62.7 � 103

E � 57.2 � 103

150�C

95�C

GENERAL NOTES:(a) See Table NFA-4 for tabular values.(b) This chart is not to be used for welded construction.

FIG. NFA-4 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 3004 IN H34 TEMPER [Notes (7) and (8)]

720



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

6.0

7.0

8.0

9.010

12

14

16

1820

30

40

50

35

25

0.00001


Up to 40�C

E � 71.0 � 103


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

6.0

7.0

8.0

9.010

12

14

16

1820

25

30

40

50

35

0.00001


Up to 40�C

205�C150�C95�C

E � 70.3 � 103

E � 67.6 � 103

E � 55.8 � 103

E � 55.2 � 103


721



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

10

1.0

2.0

3.0

4.0

5.0

6.0

7.0

8.0

9.0

2.5

3.5

1.2

1.4

1.6

1.8

0.00001

GENERAL NOTE: See Table NFA-7 for tabular values.Up to 95�C

150�C

205�C

E � 69.0 � 103

E � 62.7 � 103

E � 57.2 � 103

FIG. NFA-7 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 1060 IN O TEMPER [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

40

4.0

5.0

6.0

7.0

8.0

9.010

12

14

16

18

20

30

35

25

0.00001


Up to 40�C

150�C

205�C

95�C

E � 70.3 � 103

E � 67.6 � 103

E � 62.1 � 103

E � 55.2 � 103

FIG. NFA-8 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 5052 IN O AND H112 TEMPERS [Notes (7) and (9)]

722



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

6.0

7.0

8.0

9.010

12

14

16

1820

30

40

50

35

25

0.00001


E � 71.0 � 103


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

80

8.09.010

12

14

16

18

20

30

40

50

60

70

35

25

0.00001


E � 71.0 � 103

FIG. NFA-10 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM ALLOY 5456 IN O TEMPER [Note (7)]

723



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2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

80

8.09.010

12

14

16

18

20

30

40

50

60

70

35

25

0.00001

GENERAL NOTE: See Table NFA-11 for tabular values. Up to 65�C(1)

(3)(2)

(4)(5)

E � 71.0 � 103

(1) O, H112 (YS equal to 124 MPa)(2) O, H112 (YS equal to 117 MPa)(3) O, H112 (YS equal to 110 MPa)(4) O (YS equal to 103 MPa)(5) O (YS equal to 97 MPa)YS = yield strength


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

1009080

70

60

50

40

30

20

18

16

14

25

35

12

0.00001


Up to 95�C

150�C

205�C

E � 68.9 � 103

E � 63.4 � 103

E � 60.0 � 103

FIG. NFA-12 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF WELDED ALUMINUM ALLOY 6061-T6, -T651, -T6510, AND -T6511 WHEN WELDED

WITH 5356 OR 5556 FILLER METAL, ALL THICKNESSES; 4043 OR 5554 FILLER METAL, THICKNESS ≤ 10 mm[Note (7)]

724



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PART D — PROPERTIES (METRIC) Fig. NFC-1

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

50

40

35

25

30

20

1816

14

12

109.0

8.0

7.0

6.0

0.00001

GENERAL NOTE: See Table NFA-13 for tabular values. Up to 95�C150�C

205�C

E � 68.9 � 103

E � 63.4 � 103

E � 60.0 � 103

FIG. NFA-13 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF WELDED ALUMINUM ALLOY 6061-T4, -T451, -T4510, AND -T4511 WHEN WELDEDWITH 4043, 5554, 5356, OR 5556 FILLER METAL, ALL THICKNESSES; AND OF WELDED ALUMINUM ALLOY

6061-T6, -T651, -T6510, AND -T6511 WHEN WELDED WITH 4043 OR 5554 FILLER METAL, THICKNESS > 10 mm[Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

40

4.0

7.0

6.0

5.0

8.0

9.0

10

12

14

16

1820

25

30

35

0.00001

GENERAL NOTE: See Table NFC-1 for tabular values.

Up to 65�C

E � 110.3 � 103

FIG. NFC-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED COPPER, TYPE DHP [Note (7)]

725



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Fig. NFC-2 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

6.0

7.0

8.0

9.010

12

14

16

1820

25

30

40

50

35

0.00001

GENERAL NOTE: See Table NFC-2 for tabular values. Up to 65�C

175�C

E � 124.1 � 103

FIG. NFC-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF COPPER–SILICON ALLOYS A AND C [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

6.0

7.0

8.0

9.010

12

14

16

1820

25

30

40

50

35

0.00001


Up to 65�C

315�C205�C

E � 124.1 � 103

E � 115.8 � 103

E � 111.7 � 103

FIG. NFC-3 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED 90–10 COPPER–NICKEL ALLOY [Note (7)]

726



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Fig. NFC-5

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

8070

60

50

40

30

20

18

16

14

12

10

35

25

8.0

9.0

0.00001

GENERAL NOTE: See Table NFC-4 for tabular values.Up to 65�C

370�C

120�C

205�C

E � 151.7 � 103

E � 144.8 � 103

E � 135.8 � 103

FIG. NFC-4 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED 70–30 COPPER–NICKEL ALLOY [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

8070

60

50

40

30

20

18

16

14

12

10

35

25

8.0

9.0

0.00001


Up to 150�C

Up to 40�C

150�C

E � 115.8 � 103

E � 120.7 � 103

FIG. NFC-5 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF WELDED COPPER–IRON ALLOY TUBE C19400 (SB-543 Welded)

[Note (7)]

727



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Fig. NFC-6 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

10090

80

70

60

50

40

35

25

30

2018

16

14

12

0.00001

GENERAL NOTE: See Table NFC-6 for tabular values. Up to 93�C

149�C

Up to 95�C

150�C

E � 114.4 � 103

E � 112.4 � 103

FIG. NFC-6 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SB-75 AND SB-111 LIGHT DRAWN SEAMLESS COPPER TUBES, ALLOYS C10200,

C12000, C12200, AND C14200

0.1

7

14

21

28

35

42

0.0198765432 98765432 9876543298765432

0.001

Factor A

Fact

or

B

0.00010.00001


E = 117.2 � 103

Up to20�C

95�C

205�C

E = 112.4 � 103

E = 114.4 � 103

FIG. NFC-7 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED COPPER, SB-75, UNS C12200, TEMPER 050 [Note (1)]

728



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Fig. NFN-1

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

100

90

80

70

60

50

40

35

25

20

18

16

14

30

12

0.00001

Up to 65�C

205�C315�C

E � 124.1 � 103

E � 106.9 � 103

E � 73.8 � 103


FIG. NFC-8 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ALUMINUM BRONZE ALLOY C61400 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

50

6.0

7.0

8.0

9.010

12

14

16

18

20

25

30

40

35

0.00001

Up to 40�C

425�C

205 to 315�C

540�C

E � 206.8 � 103

E � 196.5 � 103

E � 181.3 � 103

E � 172.4 � 103

GENERAL NOTE: See Table NFN-1 for tabular values.

FIG. NFN-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF LOW CARBON NICKEL N02201 [Note (7)]

729



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Fig. NFN-2 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

60

6.0

7.0

8.0

9.010

12

14

16

18

20

25

30

40

50

35

0.00001

Up to 315�C

E � 206.8 � 103 (40�C) E � 204.1 � 103 (95�C) E � 197.2 � 103 (205�C) E � 188.9 � 103 (315�C)


FIG. NFN-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL N02200 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

16

14

12

2018

25

30

Fact

or

B

Factor A

35

40

50

60

70

8090

120

0.00001

100GENERAL NOTE: See Table NFN-3 for tabular values.

Up to 40�C

205�C

95�C

315 to 480�C

E � 178.6 � 103 (205�C)E � 168.2 � 103 (315�C)E � 153.8 � 103 (425�C)E � 141.3 � 103 (480�C)

FIG. NFN-3 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED NICKEL–COPPER ALLOY N04400 [Note (7)]

730



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

16

14

12

2018

25

30

Fact

or

B

Factor A

35

40

50

60

70

8090

120

0.00001

100GENERAL NOTE: See Table NFN-4 for tabular values. Up to 40�C 95�C

425�C

595�C

650�C

540�C205 to 315�C

E � 212.0 � 103 (to 95�C)

E � 197.2 � 103 (425�C)E � 184.8 � 103 (540�C)E � 175.8 � 103 (650�C)

E � 203.4 � 103 (205 to 315�C)

FIG. NFN-4 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED NICKEL–CHROMIUM–IRON ALLOY N06600 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

201816

30

25

35

40Fa

cto

r B

Factor A

50

60

70

9080

100

120

160

0.00001

140GENERAL NOTE: See Table NFN-5 for tabular values.Up to 40�C

205�C

315 to 345�C

E � 203.4 � 103

E � 189.6 � 103

FIG. NFN-5 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–MOLYBDENUM ALLOY N10001 [Note (7)]

731



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

201816

30

25

35

Fact

or

B

Factor A

50

60

70

8090100

120

160

0.00001

140

40

GENERAL NOTE: See Table NFN-6 for tabular values. Up to 40�C

705�C

650�C

595�C

205�C315�C

425�C

E � 220.6 � 103

E � 199.3 � 103

E � 179.3 � 103

E � 172.4 � 103

E � 161.3 � 103

E � 157.2 � 103

E � 203.4 � 103

FIG. NFN-6 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–MOLYBDENUM–CHROMIUM–IRON ALLOY N10003 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

201816

30

25

35

Fact

or

B

Factor A

50

60

70

80

90100

120

160

0.00001

140

40

GENERAL NOTE: See Table NFN-7 for tabular values.Up to 40�C

370�C205�C

100�C

E � 195.1 � 103

E � 174.4 � 103E � 184.8 � 103

FIG. NFN-7 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–IRON–CHROMIUM–MOLYBDENUM–COPPER ALLOY N08825 [Note (7)]

732



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

16

14

12

2018

25

Fact

or

B

Factor A

35

40

50

60

70

8090

120

0.00001

100

30


425�C540�C

205�C

595�C

315�C

E � 196.5 � 103

E � 171.0 � 103

E � 158.6 � 103

E � 183.4 � 103

FIG. NFN-8 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–IRON–CHROMIUM ALLOY N08800 (Annealed) [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

16

14

12

2018

25

Fact

or

B

Factor A

35

40

50

60

70

8090

120

0.00001

100

30


Up to 40�C

480�C

150�C

705�C

595�C

315�C

E � 193.1 � 103

E � 160.0 � 103

E � 146.9 � 103

E � 168.9 � 103

FIG. NFN-9 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–IRON–CHROMIUM ALLOY N08810 (Annealed) [Note (7)]

733



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

25

20

35

30

40

Fact

or

B

Factor A

60

70

90

80

100

120

140

160

200

0.00001

180

50


Up to 40�C

315�C

425�C

100�C

540�C

205�C

E � 205.5 � 103

E � 175.1 � 103E � 188.2 � 103

FIG. NFN-10 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF LOW CARBON NICKEL–MOLYBDENUM–CHROMIUM ALLOY N10276 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

2018

16

30

25

35

40

Fact

or

B

Factor A

60

70

8090100

120

160

0.00001

140

50


Up to 40�C

425 to 540�C

95�C205�C

E � 191.7 � 103

E � 161.3 � 103E � 181.3 � 103

FIG. NFN-11 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF SOLUTION TREATED NICKEL–CHROMIUM–IRON–MOLYBDENUM–COPPER ALLOYS

N06007 AND N06975 [Note (7)]

734



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

201816

30

25

35

40

Fact

or

B

Factor A

60

70

8090100

120

160

0.00001

140

50


425�C315�C

95�C

205�C

E � 208.9 � 103

E � 190.3 � 103E � 199.9 � 103

E � 175.8 � 103E � 182.0 � 103

FIG. NFN-12 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF WROUGHT CHROMIUM–NICKEL–IRON–MOLYBDENUM–COPPER–COLUMBIUM

STABILIZED ALLOY N08020 AND IRON–NICKEL–CHROMIUM–MOLYBDENUM ALLOY N08367, SB-462, SB-463,SB-464, SB-468, AND SB-473 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

2018

16

30

25

35

40

Fact

or

B

Factor A

60

70

8090100

120

160

0.00001

140

50


Up to 40�C

425�C

95�C

205�C

E � 196.5 � 103

E � 172.4 � 103E � 182.7 � 103

FIG. NFN-13 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–IRON–CHROMIUM–SILICON ALLOY N08330

735



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

160

16

1820

25

30

35

40

50

70

60

80

100

120

140

90

0.00001

95�C205�C

315�C540�C

Up to 40�CGENERAL NOTE: See Table NFN-14 for tabular values.

E � 210 � 103

E � 201 � 103

E � 179 � 103

FIG. NFN-14 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–CHROMIUM–MOLYBDENUM ALLOY N06455

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

160

16

1820

25

30

35

40

50

70

60

80

100

120

140

90

0.00001

205�C

315�C

95�C

425�C540�C

Up to 40�CGENERAL NOTE: See Table NFN-15 for tabular values.

E � 196.5 � 103 (40�C)

E � 192 � 103 (95�C)

E � 187 � 103 (205�C)

E � 182 � 103 (315�C) E � 175 � 103 (425�C)

E � 167 � 103 (540�C)


736



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

250

16

18

30

25

20

35

40

50

60

90

80

70

120

100

140

180200

160

0.00001

205�C315�C

95�C

425�C

Up to 40�C


E � 214.4 � 103 (40�C) E � 213.0 � 103 (95�C) E � 207.5 � 103 (205�C)

E � 202.0 � 103 (315�C) E � 195.8 � 103 (425�C)


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

250

20

30

25

35

40

50

60

90

80

70

120

100

140

180200

160

0.00001

260�C

Up to 40�C

425�C to 650�C


E � 207 � 103

E � 193 � 103

E � 163 � 103

E � 187 � 103

150�C

FIG. NFN-17 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ANNEALED NICKEL–CHROMIUM–MOLYBDENUM–COLUMBIUM ALLOY N06625

(SB-443, SB-444, and SB-446 in Alloy 625) [Note (7)]

737



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

140

12

18

14

20

25

30

35

50

40

70

80

100

120

90

0.00001

16

60

95�C


370�C425�C

260�C

RT

175�C

E � 196 � 103

E � 186 � 103

E � 177 � 103

95�CRT

260�C175�C

425�C370�C

FIG. NFN-18 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–MOLYBDENUM–CHROMIUM–IRON–COPPER ALLOY N06985 WHOSE

THICKNESS IS 19 mm AND UNDER HAVING A MINIMUM YIELD STRENGTH OF 240 MPa

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

140

12

18

14

20

25

30

35

50

40

70

80

100

120

90

0.00001

16

60260�C


345�C425�C

95�C

RT

175�C

E � 196 � 103

E � 186 � 103

E � 172 � 103

95�CRT

260�C175�C

425�C345�C

FIG. NFN-19 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–MOLYBDENUM–CHROMIUM–IRON–COPPER ALLOY N06985 WHOSE

THICKNESS IS GREATER THAN 19 mm HAVING A MINIMUM YIELD STRENGTH OF 207 MPa

738



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

14

1618

Fact

or

B

Factor A

120

10090

80

70

60

50

40

30

20

35

25

0.00001


Up to 40�C

205�C

205�C

E � 208 � 103

E � 193 � 103

FIG. NFN-20 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF WORK-HARDENED NICKEL [Note (10)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

14

Fact

or

B

Factor A

250

200180

160

140

120

1009080

70

60

50

40

30

35

25

201816

0.00001

Up to 40�C205�C

315�C to 480�C

E � 218 � 103

E � 206.8 � 103

E � 183.4 � 103

FIG. NFN-21 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL–CHROMIUM–IRON ALLOYS N06600 AND N06690, SB-163 (Specified Minimum

Yield Strength 276 MPa)

739



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


FIG. NFN-22 CHART FOR DETERMINING SHELL THICKNESS OF CYLINDRICAL AND SPHERICAL VESSELSUNDER EXTERNAL PRESSURE WHEN CONSTRUCTED OF SOLUTION ANNEALED Ni–Cr–Mo–Cb ALLOY,

GRADE 2 N06625 [Note (12)]

FIG. NFN-23 CHART FOR DETERMINING SHELL THICKNESS OF CYLINDRICAL AND SPHERICAL VESSELSUNDER EXTERNAL PRESSURE WHEN CONSTRUCTED OF NICKEL–IRON–CHROMIUM ALLOY 800 (Cold Worked)

740



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Fig. NFT-1

0.0001 0.001

Factor A

Fact

or

B

0.01 0.1

7

14

21

28

354249566370

140

210

280

2 98765432 98765432 9876543

Up to 20�C150�C315�C705�C870�C925�C


E = 228.9 × 103

E = 204.1 × 103

E = 190.0 × 103

E = 172.4 × 103

E = 153.1 × 103

E = 137.2 × 103

FIG. NFN-24 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF NICKEL ALLOY N06230 [Note (4)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

20

Fact

or

B

Factor A

200180

160

140

120

1009080

70

60

50

40

35

25

30

0.00001

GENERAL NOTE: See Table NFT-1 for tabular values. Up to 40�C

95�C

205�C

315�C

E � 116.5 � 103

E � 100.7 � 103

E � 89.6 � 103

E � 78.6 � 103

FIG. NFT-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF UNALLOYED TITANIUM, GRADE 3 [Note (7)]

741



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Fig. NFT-2 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

16

2018

Fact

or

B

Factor A

160140

120

1009080

70

60

50

40

35

25

30

0.00001

GENERAL NOTE: See Table NFT-2 for tabular values. Up to 40�C

95�C

205�C

315�C

E � 115.1 � 103

E � 98.6 � 103

E � 89.6 � 103

E � 77.9 � 103

FIG. NFT-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF UNALLOYED TITANIUM, GRADE 2 [Note (7)]

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

12

14

16

2018

Fact

or

B

Factor A

120

1009080

70

60

50

40

35

25

30

0.00001

GENERAL NOTE: See Table NFT-3 for tabular values.

205�C

E � 107 � 103

E � 95.1 � 103

E � 86.2 � 103

40�C

315�C

FIG. NFT-3 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF TITANIUM, GRADE 1

742



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Fig. NFZ-1

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

120

1.6

1.82.0

3.0

4.0

2.5

3.5

5.0

6.0

7.0

8.0

10

12

14

16

1820

25

30

40

50

60

80

10090

70

35

9.0

0.00001

Up to 40�C

260�C

370�C

150�C

E � 99.3 � 103

E � 92.4 � 103

E � 79.3 � 103

E � 68.3 � 103

GENERAL NOTE: See Table NFZ-1 for tabular values.

FIG. NFZ-1 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ZIRCONIUM ALLOY 702 [Note (11)]

743



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Fig. NFZ-2 2004 SECTION II

2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 9 2 3 4 5 6 7 8 90.0001 0.001 0.01 0.1

Fact

or

B

Factor A

200180

160

140

120

100

9080

70

60

50

40

35

25

30

20

0.00001

Up to 40�C

370�C

150�C

260�C

E � 66.9 � 103

E � 75.2 � 103

E � 86.2 � 103

E � 100.6 � 103

GENERAL NOTE: See Table NFZ-2 for tabular values.

FIG. NFZ-2 CHART FOR DETERMINING SHELL THICKNESS OF COMPONENTS UNDER EXTERNAL PRESSUREWHEN CONSTRUCTED OF ZIRCONIUM ALLOY 705 (R60705)

744



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC)

NOTES TO FIGURES OF SUBPART 3

GENERAL NOTE: The external pressure charts do not account for reduction of buckling strength due to creep under long-term loads. Theeffect of creep on buckling shall be considered at temperatures for which allowable stresses are shown italicized in Tables 1A and 1B.

NOTES:(1) See Tables 1A and 2A for applicable specification numbers.(2) See Table Y-1 for values of tabulated yield strength at design temperature.(3) When tabulated yield strength values are less than 260 MPa for the material covered by this chart, Fig. CS-2 may be used. (Tabulated

yield strength values take priority over specified minimum yield strength values.)(4) The external pressure chart does not account for reduction of buckling strength due to creep under long-term loads at temperatures

above 540°C.(5) See Section VIII, Division 1, Table UCI-23 for applicable specification numbers.(6) See Section VIII, Division 1, Table UCD-23 for applicable specification numbers.(7) See Tables 1B and 2B for applicable specification numbers for Section VIII, Divisions 1 and 2, respectively.(8) For Section III application, maximum use limit is 120°C, except for SB-209/3003/H112/6–12.7 and 13–75 mm use limits are 150°C

and 95°C, respectively. Use 150°C curve for interpolation only.(9) For Section III application, maximum use limit is 120°C, except for SB-210 use limit is 150°C. Use 150°C curve for interpolation only.

(10) Vessels constructed of material covered by this chart must be subjected to an external hydrostatic test pressure of three times the maximumallowable working pressure. Thicknesses determined by this chart are minimum, and greater thickness may be required to withstand thetest pressure if the planishing used does not provide an adequate degree of work-hardening.

(11) See Table 1B for applicable specification numbers.(12) The external pressure chart does not account for reduction of buckling strength due to creep under long-term loads at temperatures

above 650°C.

745



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table G 2004 SECTION II

TA

BL

EG

TA

BU

LA

RV

AL

UE

SF

OR

FIG

.G

Do/

TL

/Do

AD

o/T

L/D

oA

Do/

TL

/Do

AD

o/T

L/D

oA

Do/

TL

/Do

AD

o/T

L/D

oA

42.

20.

959

−01

83.

00.

212

−01

200.

80.

203

−01

303.

00.

246

−02

506.

00.

548

−03

804.

00.

424

−03

2.6

0.88

44.

00.

192

1.0

0.15

64.

00.

177

7.0

0.50

26.

60.

241

3.0

0.83

95.

00.

184

1.2

0.12

74.

40.

161

8.0

0.47

88.

00.

205

4.0

0.78

37.

00.

179

2.0

0.71

3−

025.

00.

147

10.0

0.45

810

.00.

186

5.0

0.75

910

.00.

176

3.0

0.44

66.

00.

136

12.0

0.44

914

.00.

176

7.0

0.73

920

.00.

174

3.4

0.38

87.

00.

130

16.0

0.44

430

.00.

172

10.0

0.72

950

.00.

174

4.0

0.34

210

.00.

125

40.0

0.44

050

.00.

172

30.0

0.72

05.

00.

308

30.0

0.12

250

.00.

440

50.0

0.72

010

0.56

0.96

4−

017.

00.

287

50.0

0.12

210

00.

050.

741

−01

0.7

0.72

010

.00.

280

600.

074

0.95

4−

010.

070.

398

51.

40.

929

−01

1.0

0.46

340

.00.

275

400.

120.

864

−01

0.10

0.55

60.

100.

220

1.6

0.80

21.

20.

371

50.0

0.27

50.

20.

385

0.14

0.32

30.

140.

133

2.0

0.65

82.

00.

201

0.3

0.22

20.

20.

193

0.20

0.83

1−

022.

40.

586

2.4

0.16

525

0.2

0.87

7−

010.

40.

155

0.4

0.81

2−

020.

400.

364

3.0

0.53

23.

00.

139

0.3

0.48

40.

60.

958

−02

0.6

0.51

00.

50.

283

4.0

0.49

44.

00.

124

0.5

0.25

00.

80.

691

0.8

0.37

10.

80.

170

5.0

0.47

85.

00.

118

0.8

0.14

31.

00.

539

1.0

0.29

11.

00.

134

7.0

0.46

57.

00.

114

1.0

0.11

11.

20.

441

2.0

0.13

82.

00.

641

−03

10.0

0.45

910

.00.

112

1.2

0.90

2−

022.

00.

252

3.0

0.88

6−

034.

00.

305

30.0

0.45

416

.00.

111

2.0

0.50

84.

00.

117

4.0

0.64

56.

00.

195

50.0

0.45

350

.00.

111

3.0

0.32

35.

00.

912

−03

6.0

0.40

98.

00.

142

3.4

0.27

86.

00.

804

7.0

0.36

410

.00.

124

61.

20.

837

−01

150.

340.

968

−01

4.0

0.23

57.

00.

756

8.0

0.34

114

.00.

114

1.6

0.58

40.

40.

770

4.4

0.21

98.

00.

731

10.0

0.32

225

.00.

110

2.0

0.46

90.

60.

453

5.0

0.20

410

.00.

708

14.0

0.31

050

.00.

110

2.4

0.41

11.

00.

244

6.0

0.19

116

.00.

692

40.0

0.30

63.

00.

369

1.2

0.19

77.

00.

186

40.0

0.68

850

.00.

306

125

0.05

0.48

0−

014.

00.

341

2.0

0.10

910

.00.

180

50.0

0.68

80.

060.

344

5.0

0.32

92.

40.

890

−02

30.0

0.17

680

0.05

40.

990

−01

0.08

0.21

07.

00.

320

3.0

0.69

150

.00.

176

500.

088

0.93

0−

010.

070.

608

0.10

0.14

810

.00.

316

4.0

0.57

30.

10.

782

0.09

0.39

10.

140.

917

−02

30.0

0.31

25.

00.

534

300.

160.

904

−01

0.2

0.26

30.

100.

328

0.2

0.57

850

.00.

312

6.0

0.51

60.

20.

635

0.3

0.15

40.

140.

196

0.4

0.25

710

.00.

497

0.3

0.35

70.

40.

108

0.20

0.12

00.

60.

165

80.

740.

968

−01

40.0

0.49

00.

40.

246

0.6

0.67

7−

020.

240.

950

−02

0.8

0.12

10.

80.

875

50.0

0.49

00.

60.

150

0.8

0.49

00.

40.

516

1.0

0.95

5−

031.

00.

660

0.8

0.10

81.

00.

384

0.6

0.32

82.

00.

459

1.6

0.37

220

0.24

0.98

2−

011.

00.

838

−02

2.0

0.18

10.

80.

239

4.0

0.22

02.

00.

285

0.4

0.47

71.

20.

683

4.0

0.84

2−

031.

00.

188

6.0

0.14

12.

40.

242

0.6

0.28

62.

00.

388

5.0

0.65

22.

00.

895

−03

9.0

0.90

4−

04

746



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Table G

TA

BL

EG

(CO

NT

’D)

TA

BU

LA

RV

AL

UE

SF

OR

FIG

.G

Do/

TL

/Do

AD

o/T

L/D

oA

Do/

TL

/Do

AD

o/T

L/D

oA

Do/

TL

/Do

AD

o/T

L/D

oA

125

10.0

0.83

7−

0420

00.

080.

909

−02

250

2.0

0.16

3−

0330

040

.00.

123

−04

500

0.6

0.19

9−

0380

00.

100.

682

−03

12.0

0.77

00.

100.

659

4.0

0.78

9−

0450

.00.

122

0.8

0.14

80.

120.

551

14.0

0.74

00.

140.

421

6.0

0.51

31.

00.

118

0.16

0.39

820

.00.

713

0.2

0.27

28.

00.

377

400

0.05

0.54

9−

022.

00.

579

−04

0.2

0.31

240

.00.

704

0.3

0.17

110

.00.

293

0.06

0.41

74.

00.

282

0.4

0.14

950

.00.

704

0.5

0.97

6−

0312

.00.

238

0.08

0.27

86.

00.

185

0.6

0.98

0−

040.

80.

592

14.0

0.21

00.

100.

208

8.0

0.13

70.

80.

728

150

0.05

0.33

8−

011.

00.

469

16.0

0.19

60.

120.

166

10.0

0.10

71.

00.

580

0.06

0.24

42.

00.

227

20.0

0.18

40.

160.

118

12.0

0.88

0−

052.

00.

286

0.08

0.15

14.

00.

110

40.0

0.17

60.

20.

914

−03

4.0

0.14

00.

100.

108

6.0

0.71

1−

0450

.00.

176

0.4

0.42

960

00.

050.

270

−02

5.0

0.11

20.

120.

833

−02

8.0

0.52

00.

60.

280

0.06

0.20

85.

60.

992

−05

0.16

0.56

910

.00.

403

300

0.05

0.92

3−

020.

80.

207

0.08

0.14

20.

20.

431

12.0

0.33

80.

060.

690

1.0

0.16

50.

100.

108

0.4

0.19

414

.00.

309

0.08

0.45

22.

00.

808

−04

0.12

0.86

8−

030.

60.

125

16.0

0.29

50.

100.

334

4.0

0.39

30.

160.

624

1.0

0.72

6−

0320

.00.

283

0.12

0.26

46.

00.

257

0.2

0.48

62.

00.

349

40.0

0.27

50.

20.

143

8.0

0.18

90.

40.

231

1000

0.05

0.11

3−

024.

00.

168

50.0

0.27

50.

40.

666

−03

10.0

0.14

80.

60.

151

0.06

0.89

1−

036.

00.

108

0.6

0.43

314

.00.

102

0.8

0.11

20.

070.

733

8.0

0.78

7−

0425

00.

050.

129

−01

0.8

0.32

116

.00.

882

−05

1.0

0.89

4−

040.

090.

541

10.0

0.61

90.

060.

955

−02

1.0

0.25

42.

00.

439

0.12

0.38

812

.00.

553

0.08

0.61

72.

00.

124

500

0.05

0.37

0−

024.

00.

216

0.16

0.28

216

.00.

510

0.10

0.45

24.

00.

602

−04

0.06

0.28

46.

00.

141

0.2

0.22

120

.00.

498

0.14

0.29

36.

00.

393

0.08

0.19

28.

00.

104

0.4

0.10

640

.00.

489

0.2

0.19

18.

00.

287

0.10

0.14

58.

40.

988

−05

0.7

0.59

6−

0450

.00.

489

0.4

0.88

1−

0310

.00.

225

0.12

0.11

61.

00.

414

0.6

0.57

214

.00.

156

0.16

0.83

0−

0380

00.

050.

165

−02

2.0

0.20

420

00.

050.

196

−01

0.8

0.42

216

.00.

142

0.2

0.64

50.

060.

129

4.0

0.10

10.

060.

143

1.0

0.33

520

.00.

130

0.4

0.30

50.

080.

892

−03

4.2

0.95

7−

05

747



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table CS-1 2004 SECTION II

TABLE CS-1TABULAR VALUES FOR FIG. CS-1

Temp., B, Temp., B,°C A MPa °C A MPa

150 1.35 −05 1.38 +006.45 −04 6.48 +017.00 6.838.00 7.249.00 7.521.00 −03 7.721.50 8.232.00 8.489.50 9.512.00 −02 9.511.00 −01 9.51

260 1.43 −05 1.38 +005.13 −04 4.83 +016.00 5.158.00 5.581.00 −03 5.861.50 6.452.50 6.861.95 −02 9.031.00 −01 9.03

370 1.57 −05 1.38 +004.13 −04 3.54 +015.00 3.836.00 4.007.00 4.218.00 4.34

370 9.00 4.481.00 −03 4.591.50 5.002.00 5.242.12 −02 7.581.00 −01 7.58

425 1.78 −05 1.38 +003.67 −04 2.87 +014.00 3.005.00 3.216.00 3.347.00 3.521.00 −03 3.861.50 4.172.00 4.412.25 −02 6.721.00 −01 6.72

480 1.88 −05 1.38 +003.31 −04 2.41 +015.00 2.727.00 2.961.00 −03 3.251.50 3.562.50 3.962.13 −02 5.861.00 −01 5.86

748



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table CS-2 PART D — PROPERTIES (METRIC) Table CS-3



150 1.76 −05 1.72 +007.83 −04 7.79 +018.00 7.869.00 8.141.00 −03 8.482.00 1.03 +023.00 1.124.00 1.165.00 1.192.50 −02 1.211.00 −01 1.21

260 1.94 −05 1.72 +006.75 −04 6.21 +019.00 6.651.00 −03 6.892.50 8.273.00 8.558.00 9.791.00 −02 1.01 +021.50 1.072.00 1.112.80 1.171.00 −01 1.17

370 2.13 −05 1.72 +005.64 −04 4.69 +011.00 −03 5.523.00 6.961.00 −02 8.342.64 9.511.00 −01 9.51

425 2.23 −05 1.72 +005.05 −04 3.94 +011.00 −03 4.901.50 5.482.00 5.793.00 6.143.19 −02 8.551.00 −01 8.55

480 2.37 −05 1.72 +004.28 −04 3.10 +011.00 −03 4.141.50 4.692.00 5.073.00 5.458.00 6.343.00 −02 7.651.00 −01 7.65


Yield Strength, B,MPa A MPa

414 4.00 −05 4.00 +001.00 −03 1.00 +021.66 1.651.00 −01 2.07

379 4.00 −05 4.00 +001.00 −03 1.00 +021.52 1.521.00 −01 1.86

345 4.00 −05 4.00 +001.00 −03 1.00 +021.38 1.381.00 −01 1.72

310 4.00 −05 4.00 +001.00 −03 1.00 +021.24 1.241.00 −01 1.55

262 to 276 4.00 −05 4.00 +001.00 −03 1.00 +021.10 1.101.00 −01 1.38

749



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table CS-4 2004 SECTION II Table CS-5



40 1.00 −05 1.03 +00(Cl. 2) 1.56 −03 1.74 +02

3.00 1.857.00 1.989.00 2.003.00 −02 2.104.00 2.121.00 −01 2.12

40 1.00 −05 1.03 +00(Cl. 1) 1.36 −03 1.49 +02

4.00 1.611.00 −02 1.683.00 1.741.00 −01 1.74

150 1.00 −05 9.79 −01(Cl. 2) 1.35 −03 1.41 +02

6.00 1.591.00 −02 1.654.00 1.771.00 −01 1.84

150 1.00 −05 9.79 −01(Cl. 1) 1.18 −03 1.22 +02

3.00 1.294.00 1.313.00 −02 1.397.00 1.411.00 −01 1.41



40 1.99 −04 2.07 +011.60 −03 1.69 +022.00 1.703.00 1.715.00 1.726.00 1.725.00 −02 1.72

95 2.00 −04 2.07 +011.57 −03 1.62 +025.00 −02 1.62

150 2.03 −04 2.07 +011.50 −03 1.52 +023.00 1.556.00 1.555.00 −02 1.55

205 2.10 −04 2.07 +011.54 −03 1.43 +02

205 3.00 1.467.00 1.529.00 1.521.00 −02 1.545.00 1.54

290 2.15 −04 2.07 +011.08 −03 1.03 +022.00 1.134.00 1.271.00 −02 1.382.00 1.435.00 1.47

345 2.20 −04 2.07 +011.21 −03 1.03 +022.00 1.134.00 1.231.00 −02 1.345.00 1.43

750



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table CS-6 PART D — PROPERTIES (METRIC) Table HT-2



40 1.50 −04 1.52 +012.00 2.073.00 3.106.00 4.148.00 4.482.00 −03 5.524.20 6.214.00 −02 6.897.00 6.89

95 1.50 −04 1.52 +012.00 2.074.20 3.458.00 4.141.50 −03 4.83

95 4.00 5.522.00 −02 6.21

150 1.50 −04 1.52 +012.00 2.075.00 3.451.00 −03 4.142.50 4.839.00 5.522.50 −02 5.72

205 1.80 −04 1.72 +013.00 2.761.00 −03 3.797.00 4.832.50 −02 5.17

TABLE HT-1TABULAR VALUES FOR FIG. HT-1


Up to 1.00 −05 1.01 +0095 2.45 −03 2.54 +02

4.00 2.807.00 3.041.00 −02 3.172.00 3.325.00 3.45

205 1.00 −05 9.45 −012.45 −03 2.39 +024.00 2.65

205 7.00 2.901.00 −02 3.044.00 3.32

345 1.00 −05 8.55 −012.43 −03 2.17 +024.00 2.467.00 2.751.00 −02 2.883.00 3.20

TABLE HT-2TABULAR VALUES FOR FIG. HT-2


40 3.37 −04 3.45 +012.83 −03 2.90 +024.00 2.986.00 3.038.00 3.091.00 −02 3.131.50 3.232.00 3.28

40 2.50 3.323.00 3.364.00 3.415.00 3.436.00 3.437.00 3.451.00 −01 3.45

751



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table HA-1 2004 SECTION II

TABLE HA-1TABULAR VALUES FOR FIG. HA-1


40 1.42 −05 1.38 +004.63 −04 4.48 +011.50 −03 7.312.00 7.933.00 8.621.00 −02 9.656.31 1.09 +021.00 −01 1.09

205 1.59 −05 1.38 +003.91 −04 3.45 +012.00 −03 5.653.00 6.274.00 6.685.00 6.891.00 −02 7.315.38 8.001.00 −01 8.00

370 1.70 −05 1.38 +003.38 −04 2.76 +014.00 2.995.00 3.256.00 3.451.00 −03 3.972.00 4.60

370 5.00 5.276.00 5.381.00 −02 5.585.42 6.211.00 −01 6.21

480 1.81 −05 1.38 +003.15 −04 2.41 +014.00 2.665.00 2.871.50 −03 3.783.00 4.221.00 −02 4.872.00 5.127.84 5.471.00 −01 5.47

650 2.00 −05 1.38 +002.83 −04 1.96 +011.00 −03 2.872.00 3.335.00 3.821.00 −02 4.102.00 4.384.88 4.621.00 −01 4.62

752



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table HA-2 PART D — PROPERTIES (METRIC) Table HA-3



40 1.84 −05 1.72 +006.05 −04 5.79 +011.50 −03 7.652.00 8.072.50 8.413.00 8.694.00 8.965.00 9.177.00 9.381.00 −02 9.652.00 1.01 +027.26 1.081.00 −01 1.08

205 1.99 −05 1.72 +005.85 −04 5.17 +011.00 −03 6.001.50 6.692.00 7.173.00 7.724.00 8.075.00 8.276.00 8.411.00 −02 8.765.74 9.861.00 −01 9.86

370 2.18 −05 1.72 +005.33 −04 4.31 +01

370 7.00 4.831.00 −03 5.383.00 6.894.00 7.241.00 −02 7.865.00 8.765.92 8.891.00 −01 8.89

480 2.28 −05 1.72 +005.10 −04 3.90 +016.00 4.211.00 −03 4.963.00 6.244.00 6.481.00 −02 7.105.22 8.071.00 −01 8.07

650 2.47 −05 1.72 +004.60 −04 3.21 +011.00 −03 4.142.00 4.963.00 5.384.00 5.655.00 5.791.00 −02 6.177.00 6.891.00 −01 6.89



40 1.39 −05 1.38 +005.35 −04 5.21 +012.00 −03 6.966.00 8.554.00 −02 1.03 +021.00 −01 1.03

205 1.58 −05 1.38 +003.61 −04 3.19 +011.00 −03 3.791.00 −02 5.622.83 6.721.00 −01 6.72

315 1.65 −05 1.38 +003.19 −04 2.68 +011.00 −03 3.281.00 −02 4.902.81 5.831.00 −01 5.83

425 1.74 −05 1.38 +002.75 −04 2.19 +011.50 −03 2.941.00 −02 4.073.00 4.961.00 −01 4.96

753



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table HA-4 2004 SECTION II Table HA-5



40 1.43 −05 1.38 +006.00 −04 5.79 +017.00 −03 9.171.00 −02 9.652.00 1.05 +025.00 1.121.00 −01 1.12

150 1.53 −05 1.38 +004.75 −04 4.31 +015.00 −03 6.866.00 7.031.00 −02 7.584.58 8.691.00 −01 8.69

205 1.54 −05 1.38 +004.10 −04 3.71 +01

205 7.00 −03 6.171.00 −02 6.484.29 7.311.00 −01 7.31

315 1.69 −05 1.38 +003.63 −04 3.02 +015.00 −03 4.961.00 −02 5.454.56 6.211.00 −01 6.21

425 1.76 −05 1.38 +003.17 −04 2.50 +015.00 −03 4.101.00 −02 4.554.68 5.311.00 −01 5.31



20 0.000141 140.00134 131 P.L.0.0015 1330.002 1420.0025 1550.003 1640.004 1790.006 1950.01 2100.015 2170.021 225

205 0.0001509 140.001166 107 P.L.0.0015 1090.002 1140.0025 1210.003 126

205 0.004 1340.006 1450.01 1550.015 1600.023 165

345 0.00016 140.0012 103 P.L.0.0015 1070.002 1120.0025 1170.003 1230.004 1310.006 1400.01 1510.015 1550.034 157

754



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Table HA-6



20 7.07 −05 6.89 +005.00 −04 4.88 +011.00 −03 9.721.44 1.24 +021.81 1.304.48 1.399.42 1.441.89 −02 1.495.00 1.551.00 −01 1.55

95 7.25 −05 6.89 +005.00 −04 4.76 +019.71 8.481.37 −03 9.451.95 1.00 +024.81 1.109.81 1.171.96 −02 1.235.00 1.271.00 −01 1.27

205 7.55 −05 6.89 +005.00 −04 4.56 +019.76 7.451.31 −03 7.861.97 8.204.44 8.769.57 9.171.99 −02 9.515.00 9.931.00 −01 9.93

345 7.98 −05 6.89 +004.99 −04 4.31 +018.85 6.151.44 −03 6.651.81 6.834.66 7.389.80 7.722.00 −02 8.145.00 8.271.00 −01 8.27

510 8.62 −05 6.89 +004.99 −04 3.99 +019.64 6.101.09 −03 6.241.27 6.384.84 7.109.68 7.451.99 −02 7.725.00 7.931.00 −01 7.93

650 9.64 −05 6.89 +004.98 −04 3.56 +019.32 5.551.38 −03 6.001.90 6.254.88 6.789.94 7.171.94 −02 7.455.00 7.791.00 −01 7.79

755



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table HA-7 2004 SECTION II Table HA-8



20 7.00 −05 6.89 +005.00 −04 5.03 +017.50 7.581.00 −03 1.01 +021.25 1.261.50 1.511.74 1.751.98 1.992.89 2.714.07 2.966.41 3.137.49 3.171.57 −02 3.355.00 3.591.00 −01 3.62

150 7.00 −05 6.89 +005.00 −04 4.81 +017.50 7.241.00 −03 9.581.25 1.20 +021.50 1.441.74 1.671.98 1.892.71 2.324.62 2.626.19 2.727.63 2.781.99 −02 3.015.00 3.191.00 −01 3.21



20 7.07 −05 6.89 +004.03 −04 3.92 +016.06 5.808.36 7.651.13 −03 9.581.48 1.12 +021.64 1.171.82 1.233.46 1.564.87 1.727.30 1.929.89 2.062.00 −02 2.245.00 2.241.00 −01 2.24

100 7.27 −05 6.89 +004.73 −04 4.49 +017.07 6.719.50 8.621.25 −03 1.04 +021.46 1.141.74 1.231.95 1.28

100 3.37 1.524.76 1.617.42 1.709.85 1.771.99 −02 1.925.00 1.941.00 −01 1.94

400 8.78 −05 6.89 +005.00 −04 4.21 +017.50 6.321.00 −03 8.271.25 9.651.47 1.07 +021.70 1.151.92 1.213.29 1.434.99 1.477.36 1.509.37 1.521.97 −02 1.595.00 1.641.00 −01 1.65

756



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table CI-1 PART D — PROPERTIES (METRIC) Table CD-1

TABLE CI-1TABULAR VALUES FOR FIG. CI-1


Class 60 1.00 −05 7.58 −01up to 345 1.60 −03 1.25 +02

1.00 −01 1.25

Class 50 1.00 −05 6.87 −01up to 345 1.47 −03 1.03 +02

1.00 −01 1.03

Class 40 1.00 −05 6.01 −01up to 345 1.35 −03 8.27 +01

1.00 −01 8.27

Class 30 1.00 −05 4.94 −01up to 345 1.22 −03 6.26 +01

1.00 −01 6.26

Class 20 1.00 −05 4.10 −01up to 345 9.91 −04 4.19 +01

1.00 −01 4.19

TABLE CD-1TABULAR VALUES FOR FIG. CD-1


Up to 40 1.00 −05 8.41 −011.24 −03 1.03 +022.00 1.094.00 1.191.00 −02 1.322.50 1.43

205 1.00 −05 8.41 −011.07 −03 8.96 +012.00 1.02 +023.00 1.084.00 1.131.00 −02 1.24

205 3.00 1.346.00 1.40

345 1.00 −05 7.72 −018.92 −04 6.77 +012.00 −03 8.204.00 9.516.00 1.01 +028.00 1.051.00 −02 1.072.00 1.124.00 1.17

757



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFA-1 2004 SECTION II

TABLE NFA-1TABULAR VALUES FOR FIG. NFA-1


40 1.00 −05 3.46 −011.48 −04 5.12 +002.00 6.562.50 7.383.00 8.001.00 −03 1.08 +011.50 1.184.00 1.431.00 −02 1.701.50 1.814.00 2.081.00 −01 2.08

95 1.03 −05 3.45 −011.48 −04 4.89 +002.00 6.272.50 7.033.00 7.584.00 8.341.00 −03 1.02 +013.00 1.266.00 1.432.00 −02 1.724.00 1.921.00 −01 1.92

150 1.10 −05 3.45 −011.48 −04 4.69 +002.00 5.802.50 6.543.00 7.034.00 7.727.00 8.762.50 −03 1.08 +014.00 −02 1.591.00 −01 1.59

205 1.19 −05 3.45 −019.98 2.95 +001.50 −04 4.302.00 5.262.50 5.943.00 6.394.00 6.895.00 7.241.00 −03 8.343.00 9.861.00 −02 1.13 +014.00 1.321.00 −01 1.32

758



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Table NFA-2



40 1.00 −05 3.45 −014.05 −04 1.38 +015.00 1.716.00 2.017.00 2.288.00 2.529.00 2.761.00 −03 2.941.50 3.592.00 4.032.50 4.293.00 4.504.00 4.795.00 5.016.00 5.101.00 −02 5.472.00 5.824.00 6.105.00 6.191.00 −01 6.19

95 1.02 −05 3.45 −013.01 −04 9.86 +006.00 1.82 +017.00 2.061.00 −03 2.631.50 3.232.00 3.622.50 3.903.00 4.084.00 4.305.00 4.456.00 4.541.00 −02 4.795.00 5.521.00 −01 5.52

150 1.10 −05 3.45 −011.99 −04 6.21 +002.50 7.653.00 9.244.00 1.16 +015.00 1.366.00 1.547.00 1.681.00 −03 2.061.50 2.482.50 2.933.00 3.104.00 3.345.00 3.501.00 −02 3.881.50 4.081.00 −01 4.08

205 1.18 −05 3.45 −011.47 −04 4.16 +002.00 5.482.50 6.573.00 7.454.00 8.835.00 1.00 +011.00 −03 1.381.50 1.612.00 1.792.50 1.923.00 2.035.00 2.306.00 2.367.00 2.411.00 −02 2.541.50 2.652.00 2.702.50 2.751.00 −01 2.75

759



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 1.00 −05 3.49 −013.53 −04 1.23 +014.00 1.345.00 1.506.00 1.607.00 1.688.00 1.731.00 −03 1.821.50 1.941.50 −02 2.921.00 −01 2.92

95 1.04 −05 3.45 −013.75 −04 1.23 +014.00 1.295.00 1.446.00 1.557.00 1.648.00 1.701.00 −03 1.801.50 1.941.50 −02 2.921.00 −01 2.92

150 1.07 −05 3.45 −013.48 −04 1.10 +014.00 1.245.00 1.416.00 1.527.00 1.618.00 1.681.00 −03 1.771.50 1.941.50 −02 2.921.00 −01 2.92

205 1.16 −05 3.45 −013.34 −04 9.72 +004.00 1.16 +015.00 1.366.00 1.497.00 1.588.00 1.659.00 1.711.00 −03 1.761.50 1.941.50 −02 2.921.00 −01 2.92

760



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFA-4 PART D — PROPERTIES (METRIC) Table NFA-5



40 1.00 −05 3.50 −011.26 −03 4.50 +011.50 5.142.00 6.032.50 6.543.00 6.884.00 7.245.00 7.526.00 7.721.00 −02 8.071.50 8.202.50 8.414.00 8.551.00 −01 8.55

95 1.01 −05 3.45 −011.31 −03 4.50 +011.50 4.962.00 5.772.50 6.253.00 6.604.00 6.965.00 7.246.00 7.457.00 7.581.00 −02 7.792.50 8.143.00 8.204.00 8.271.00 −01 8.27

150 1.07 −05 3.45 −016.98 −04 2.28 +011.00 −03 3.101.50 3.992.00 4.522.50 4.903.00 5.124.00 5.395.00 5.606.00 5.731.00 −02 6.011.50 6.211.00 −01 6.21

205 1.17 −05 3.45 −012.48 −04 7.31 +003.00 8.694.00 1.10 +015.00 1.286.00 1.427.00 1.549.00 1.751.00 −03 1.851.50 2.172.00 2.412.50 2.603.00 2.724.00 2.941.00 −02 3.531.50 3.791.00 −01 3.79



40 1.00 −05 3.54 −014.92 −04 1.76 +016.00 2.077.00 2.258.00 2.39

40 9.00 2.481.00 −03 2.531.71 −02 3.791.00 −01 3.79

761



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFA-6 2004 SECTION II Table NFA-7



Up to 40 1.00 −05 3.61 −016.87 −04 2.45 +018.00 2.809.00 3.031.00 −03 3.141.50 3.432.00 3.533.00 3.621.00 −02 3.933.00 4.21

95 1.01 −05 3.45 −014.99 −04 1.68 +017.00 2.228.00 2.449.00 2.631.00 −03 2.741.50 3.082.00 3.253.00 3.451.00 −02 3.903.00 4.21

150 1.10 −05 3.45 −014.99 −04 1.57 +016.00 1.827.00 2.038.00 2.211.00 −03 2.451.50 2.812.00 2.983.00 3.171.00 −02 3.593.00 3.87

205 1.26 −05 3.45 −013.98 −04 1.10 +015.00 1.307.00 1.651.00 −03 2.031.50 2.422.00 2.623.00 2.835.00 3.051.00 −02 3.262.50 3.52



95 1.01 −05 3.45 −019.01 3.21 +005.00 −04 4.837.00 5.181.50 −03 6.074.00 7.247.00 7.931.00 −02 8.271.50 8.482.00 8.621.00 −01 8.62

150 1.12 −05 3.45 −018.85 2.86 +005.00 −04 4.10

150 7.00 4.371.50 −03 4.993.00 5.506.00 5.941.00 −02 6.251.00 −01 6.25

205 1.19 −05 3.45 −017.46 2.25 +001.50 −03 4.163.00 4.695.00 4.967.00 5.079.00 5.141.00 −01 5.14

762



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




95 1.04 −05 3.45 −012.83 −04 9.72 +003.00 1.02 +014.00 1.251.00 −03 1.832.50 2.445.00 2.866.00 2.957.00 3.028.00 3.069.00 3.121.00 −02 3.141.50 3.282.00 3.351.00 −01 3.35

150 1.10 −05 3.45 −013.38 −04 1.05 +014.00 1.211.00 −03 1.832.50 2.445.00 2.866.00 2.957.00 3.02

150 8.00 3.069.00 3.121.00 −02 3.141.50 3.282.00 3.351.00 −01 3.35

205 1.23 −05 3.45 −012.88 −04 8.00 +003.00 8.344.00 1.05 +016.00 1.361.00 −03 1.652.50 2.213.00 2.324.00 2.485.00 2.616.00 2.687.00 2.768.00 2.839.00 2.881.00 −02 2.921.00 −01 2.92



65 1.00 −05 3.45 −017.92 −04 2.81 +019.00 2.991.00 −03 3.131.50 3.48

65 2.00 3.664.00 4.066.00 4.312.00 −02 4.931.00 −01 4.93



40 1.00 −05 3.57 −011.34 −03 4.99 +011.50 5.352.00 5.792.50 5.923.00 6.015.00 6.12

40 1.00 −02 6.211.50 6.282.50 6.313.00 6.344.00 6.355.00 6.381.00 −01 6.38

763



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




65 1.00 −05 3.51 −01(Curve 1) 3.01 −04 1.08 +01

5.00 1.786.00 2.127.00 2.431.00 −03 3.191.50 3.842.00 4.232.50 4.503.00 4.734.00 5.035.00 5.239.00 5.761.50 −02 6.161.74 6.251.00 −01 6.25

65 1.00 −05 3.51 −01(Curve 2) 3.01 −04 1.08 +01

5.00 1.788.00 2.581.00 −03 2.961.50 3.622.00 3.962.50 4.233.00 4.434.00 4.735.00 4.949.00 5.451.00 −02 5.531.74 5.941.00 −01 5.94

65 1.00 −05 3.51 −01(Curve 3) 3.01 −04 1.08 +01

5.00 1.736.00 2.007.00 2.251.00 −03 2.801.50 3.392.00 3.71

65 2.50 3.95(Curve 3) 3.00 4.16

9.00 5.101.00 −02 5.191.74 5.591.00 −01 5.59

65 1.00 −05 3.51 −01(Curve 4) 3.01 −04 1.08 +01

5.00 1.696.00 1.957.00 2.181.00 −03 2.701.50 3.212.00 3.522.50 3.753.00 3.924.00 4.189.00 4.781.00 −02 4.871.50 5.161.74 5.191.00 −01 5.19

65 1.00 −05 3.51 −01(Curve 5) 3.01 −04 1.08 +01

5.00 1.666.00 1.907.00 2.101.00 −03 2.561.50 3.032.00 3.312.50 3.503.00 3.684.00 3.909.00 4.451.00 −02 4.541.50 4.811.74 4.871.00 −01 4.87

764



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




Up to 95 1.00 −05 3.48 −011.19 −03 4.23 +011.50 5.032.00 5.822.50 6.203.00 6.434.00 6.677.00 6.891.00 −02 7.032.00 7.17

150 1.07 −05 3.45 −011.22 −03 4.05 +011.50 4.702.00 5.422.50 5.78

150 3.00 6.014.00 6.245.00 6.341.00 −02 6.522.50 6.65

205 1.14 −05 3.45 −018.91 −04 2.79 +011.00 −03 3.051.50 3.762.00 4.103.00 4.545.00 4.901.00 −02 5.173.00 5.43



Up to 95 1.00 −05 3.45 −017.87 −04 2.81 +019.00 3.141.00 −03 3.451.50 4.302.00 4.632.50 4.803.00 4.914.00 5.041.00 −02 5.232.50 5.39

150 1.07 −05 3.45 −017.87 −04 2.65 +011.00 −03 3.211.50 4.032.00 4.342.50 4.473.00 4.53

150 5.00 4.711.00 −02 4.873.00 5.01

205 1.13 −05 3.45 −014.95 −04 1.55 +016.00 1.857.00 2.098.00 2.291.00 −03 2.571.50 2.972.00 3.192.50 3.333.00 3.434.00 3.565.00 3.651.00 −02 3.832.50 3.93

765



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFC-1 2004 SECTION II Table NFC-3

TABLE NFC-1TABULAR VALUES FOR FIG. NFC-1

Temp., B,°C A MPa

65 1.00 −05 5.50 −011.63 −04 9.24 +002.50 1.04 +015.00 1.251.00 −03 1.484.00 2.012.50 −02 3.001.00 −01 3.00



65 1.00 −05 6.27 −015.24 −04 3.34 +014.00 −03 4.211.00 −02 4.612.00 4.902.50 4.993.00 5.054.00 5.145.00 5.216.00 5.257.00 5.301.00 −01 5.30

175 1.00 −05 6.27 −013.76 −04 2.39 +015.00 2.536.00 2.637.00 2.714.00 −03 3.611.00 −02 4.203.00 4.851.00 −01 4.85



65 1.00 −05 6.20 −013.86 −04 2.43 +013.00 −03 3.444.00 3.595.00 3.691.00 −02 3.912.00 4.082.50 4.115.00 4.221.00 −01 4.22

205 1.00 −05 5.77 −013.58 −04 2.12 +013.00 −03 3.124.00 3.251.00 −02 3.581.50 3.702.00 3.795.00 4.021.00 −01 4.02

315 1.00 −05 5.54 −011.89 −04 1.06 +012.00 1.072.50 1.143.00 1.214.00 1.345.00 1.486.00 1.611.00 −03 2.071.50 2.392.00 2.582.50 2.703.00 2.814.00 2.961.00 −02 3.283.00 3.594.00 3.651.00 −01 3.65

766



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFC-4 PART D — PROPERTIES (METRIC) Table NFC-5



65 1.00 −05 7.93 −012.30 −04 1.73 +014.00 2.345.00 2.596.00 2.791.00 −03 3.351.50 3.803.00 4.414.00 4.657.00 5.041.00 −02 5.272.00 5.724.00 6.031.00 −01 6.03

120 1.00 −05 7.45 −012.48 −04 1.73 +013.00 1.934.00 2.225.00 2.427.00 2.711.00 −03 3.011.50 3.362.00 3.613.00 3.924.00 4.147.00 4.521.00 −02 4.711.50 4.963.00 5.294.00 5.341.00 −01 5.34

205 1.00 −05 7.45 −012.48 −04 1.73 +013.00 1.944.00 2.185.00 2.347.00 2.591.00 −03 2.831.50 3.132.00 3.352.50 3.473.00 3.596.00 4.031.00 −02 4.302.00 4.594.00 4.711.00 −01 4.74

370 1.00 −05 6.81 −012.69 −04 1.73 +013.00 1.814.00 2.025.00 2.187.00 2.371.00 −03 2.581.50 2.822.00 2.982.50 3.083.00 3.176.00 3.321.00 −02 3.632.00 3.701.00 −01 3.72



40 1.50 −04 9.03 +002.00 1.21 +012.50 1.513.00 1.813.25 1.974.00 2.071.00 −03 2.724.00 4.145.00 4.416.00 4.55

40 8.00 4.831.00 −02 5.001.50 5.271.90 5.31

150 1.50 −04 8.69 +002.00 1.16 +012.50 1.453.00 1.743.45 2.00

767



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFC-6 2004 SECTION II Table NFC-7



95 3.01 −04 1.72 +016.69 3.831.00 −03 4.482.00 5.654.00 6.896.00 7.588.00 8.171.00 −02 8.552.00 9.584.00 1.03 +026.00 1.03

150 3.07 −04 1.72 +014.42 2.487.00 3.141.00 −03 3.722.00 4.964.00 6.216.00 6.898.00 7.311.00 −02 7.652.00 8.414.00 8.836.00 8.96



20 1.18 −05 6.89 −011.00 −04 5.61 +002.00 1.12 +013.00 1.684.00 1.996.00 2.178.00 2.261.00 −03 2.321.25 2.381.50 2.421.75 2.462.00 2.483.50 2.615.00 2.687.50 2.761.00 −02 2.822.00 2.963.71 3.10

95 1.20 −05 6.89 −011.00 −04 5.34 +002.00 1.06 +013.00 1.524.00 1.656.00 1.778.00 1.831.00 −03 1.881.25 1.93

95 1.50 1.961.75 1.992.00 2.013.50 2.105.00 2.167.50 2.231.00 −02 2.282.00 2.413.71 2.52

205 1.23 −05 6.89 −011.00 −04 5.19 +002.00 1.03 +013.00 1.414.00 1.506.00 1.618.00 1.661.00 −03 1.701.25 1.741.50 1.771.75 1.792.00 1.813.50 1.905.00 1.967.50 2.021.00 −02 2.062.00 2.173.67 2.28

768



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFC-8 PART D — PROPERTIES (METRIC) Table NFN-1



65 1.00 −05 6.31 −015.85 −04 3.79 +017.00 4.388.00 4.851.00 −03 5.521.50 6.452.00 6.963.00 7.524.00 7.867.00 8.341.00 −02 8.621.50 8.833.00 9.035.00 9.171.00 −01 9.17

205 1.00 −05 5.29 −015.85 −04 3.18 +017.00 3.688.00 4.121.00 −03 4.761.51 5.71

205 2.00 6.253.00 6.844.00 7.247.00 7.861.00 −02 8.141.50 8.413.00 8.894.00 9.031.00 −01 9.03

315 1.00 −05 3.65 −017.88 −04 2.91 +019.00 3.281.00 −03 3.541.50 4.582.00 5.162.50 5.544.00 6.296.00 6.841.00 −02 7.452.50 8.341.00 −01 8.34

TABLE NFN-1TABULAR VALUES FOR FIG. NFN-1


40 1.00 −05 1.05 +001.97 −04 2.10 +011.00 −03 2.791.00 −02 4.141.65 4.521.00 −01 4.52

205 1.00 −05 9.79 −012.01 −04 2.01 +011.00 −03 2.681.00 −02 4.081.84 4.521.00 −01 4.52

315 1.00 −05 9.79 −012.01 −04 2.01 +011.00 −03 2.68

315 1.00 −02 4.081.84 4.521.00 −01 4.52

425 1.00 −05 9.10 −011.87 −04 1.74 +011.00 −03 2.321.00 −02 3.433.00 4.161.00 −01 4.16

540 1.00 −05 8.62 −011.62 −04 1.41 +011.00 −03 1.981.00 −02 3.063.00 3.771.00 −01 3.77

769



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFN-2 2004 SECTION II



40 1.00 −05 1.05 +002.57 −04 2.80 +015.00 3.031.78 −02 4.731.00 −01 4.73

95 1.00 −05 1.02 +002.65 −04 2.79 +015.00 3.031.78 −02 4.731.00 −01 4.73

205 1.00 −05 9.86 −012.76 −04 2.79 +015.00 3.031.78 −02 4.731.00 −01 4.73

315 1.01 −05 9.51 −012.91 −04 2.79 +015.00 3.031.78 −02 4.731.00 −01 4.73

770



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

PART D — PROPERTIES (METRIC) Table NFN-3



40 1.00 −05 9.10 −015.23 −04 4.97 +017.00 5.321.00 −03 5.862.00 6.812.50 7.103.00 7.385.00 8.006.00 8.207.00 8.348.00 8.411.00 −02 8.622.00 8.962.50 9.104.00 9.171.00 −01 9.17

95 1.00 −05 9.10 −014.68 −04 4.43 +016.00 4.679.00 5.141.00 −03 5.291.50 5.752.00 6.073.00 6.554.00 6.865.00 7.107.00 7.381.00 −02 7.651.50 7.932.50 8.144.00 8.271.00 −01 8.27

205 1.00 −05 9.10 −014.23 −04 4.01 +017.00 4.501.00 −03 4.911.50 5.352.50 5.893.00 6.084.00 6.406.00 6.787.00 6.899.00 7.101.00 −02 7.171.50 7.38

205 2.00 7.583.00 7.721.00 −01 7.72

315 1.00 −05 8.41 −014.37 −04 3.87 +015.00 3.961.00 −03 4.652.00 5.353.00 5.814.00 6.056.00 6.468.00 6.671.00 −02 6.851.50 7.102.00 7.243.00 7.381.00 −01 7.38

425 1.00 −05 7.58 −015.00 −04 3.96 +011.00 −03 4.652.00 5.353.00 5.814.00 6.056.00 6.468.00 6.671.00 −02 6.851.50 7.102.00 7.243.00 7.381.00 −01 7.38

480 1.00 −05 6.88 −015.28 −04 3.90 +011.00 −03 4.562.00 5.333.00 5.814.00 6.056.00 6.468.00 6.641.00 −02 6.851.50 7.102.00 7.243.00 7.381.00 −01 7.38

771



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFN-4 2004 SECTION II Table NFN-5



40 1.00 −05 1.10 +005.31 −04 5.96 +011.00 −03 6.783.00 8.074.00 8.411.00 −02 9.172.00 9.511.00 −01 9.51

95 1.00 −05 1.10 +004.94 −04 5.46 +011.00 −03 6.252.00 7.033.00 7.459.00 8.342.00 −02 8.691.00 −01 8.83

205 1.00 −05 1.03 +005.00 −04 5.30 +011.00 −03 6.092.00 6.794.00 7.455.00 7.651.00 −02 8.073.00 8.481.00 −01 8.48

315 1.00 −05 1.03 +005.00 −04 5.30 +011.00 −03 6.092.00 6.79

315 4.00 7.455.00 7.651.00 −02 8.073.00 8.481.00 −01 8.48

425 1.00 −05 9.93 −014.87 −04 4.98 +011.00 −03 5.754.00 7.031.50 −02 7.863.00 8.141.00 −01 8.14

540 1.00 −05 9.31 −014.71 −04 4.50 +011.00 −03 5.242.00 5.835.00 6.491.00 −02 6.853.00 7.311.00 −01 7.31

595 1.00 −05 8.83 −013.72 −04 3.35 +014.00 3.351.00 −01 3.35

650 1.00 −05 8.83 −012.50 −04 2.26 +011.00 −01 2.26



40 1.00 −05 1.02 +005.51 −04 5.86 +012.50 −03 1.08 +023.00 1.154.00 1.235.00 1.287.00 1.321.00 −02 1.355.00 1.471.00 −01 1.47

205 1.00 −05 1.02 +005.09 −04 5.40 +014.00 −03 9.795.00 1.03 +029.00 1.111.50 −02 1.14

205 2.50 1.171.00 −01 1.17

315–345 1.00 −05 9.45 −013.12 −04 3.01 +019.00 −03 5.061.50 6.612.00 7.452.50 8.073.00 8.414.00 8.965.00 9.317.00 9.721.00 −02 1.01 +021.50 1.042.50 1.071.00 −01 1.07

772



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFN-6 PART D — PROPERTIES (METRIC) Table NFN-7



40 1.00 −05 1.11 +008.79 −04 1.01 +021.00 −03 1.031.00 −02 1.371.50 1.40

205 1.00 −05 1.01 +008.47 −04 8.89 +011.00 −03 9.033.00 9.931.00 −02 1.09 +024.00 1.16

315 1.00 −05 9.79 −018.20 −04 8.34 +011.00 −03 8.555.00 9.651.00 −02 1.00 +023.00 1.031.00 −01 1.07

425 1.00 −05 8.89 −018.51 −04 7.86 +01

425 1.00 −03 8.002.00 8.484.00 8.891.00 −02 9.315.00 9.93

595 1.00 −05 8.55 −017.86 −04 6.96 +011.00 −03 7.172.00 7.584.00 8.001.00 −02 8.272.00 8.486.00 8.69

650 1.00 −05 8.00 −018.39 −04 6.85 +011.00 −01 6.85

705 1.00 −05 7.72 −014.93 −04 3.91 +011.00 −01 3.91



40 1.00 −05 9.65 −018.25 −04 8.34 +011.00 −03 8.552.00 9.176.00 1.04 +021.00 −02 1.102.00 1.192.50 1.23

95 1.00 −05 9.86 −017.77 −04 7.79 +011.00 −03 8.004.00 9.171.00 −02 9.934.00 1.08 +02

205 1.00 −05 9.10 −017.45 −04 7.17 +011.00 −03 7.314.00 8.001.00 −02 8.484.00 9.24

370 1.00 −05 8.62 −017.22 −04 6.57 +011.00 −03 6.672.00 6.898.00 7.452.00 −02 7.796.00 8.27

773



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 1.00 −05 9.86 −017.79 −04 8.07 +011.00 −03 8.342.00 9.174.00 9.721.00 −02 1.02 +024.00 1.061.00 −01 1.06

205 1.00 −05 9.10 −017.37 −04 7.03 +011.00 −03 7.244.00 8.141.00 −02 8.623.00 9.031.00 −01 9.03

315 1.00 −05 9.10 −016.97 −04 6.60 +011.00 −03 6.803.00 7.521.00 −02 8.143.00 8.621.00 −01 8.62

425 1.00 −05 8.41 −016.87 −04 6.10 +011.00 −03 6.382.00 6.764.00 7.101.00 −02 7.522.50 7.861.00 −01 7.86

540 1.00 −05 7.86 −016.72 −04 5.52 +011.00 −03 5.872.00 6.434.00 6.871.00 −02 7.243.00 7.651.00 −01 7.65

595 1.00 −05 7.86 −015.26 −04 4.31 +011.00 −03 5.052.00 5.744.00 6.231.00 −02 6.802.50 7.311.00 −01 7.31



40 1.00 −05 9.65 −014.92 −04 4.94 +011.00 −03 5.742.00 6.545.00 7.451.00 −02 8.002.50 8.69

150 1.00 −05 9.65 −014.36 −04 4.36 +016.00 4.798.00 5.141.00 −03 5.304.00 5.871.00 −02 6.272.50 6.70

315 1.00 −05 8.41 −014.18 −04 3.64 +011.00 −03 4.03

315 5.00 4.891.00 −02 5.322.00 5.76

480 1.00 −05 8.41 −014.18 −04 3.64 +011.00 −03 3.945.00 4.591.00 −02 4.902.00 5.24

595 1.00 −05 7.86 −014.30 −04 3.55 +011.00 −03 3.771.00 −02 4.454.00 4.94

705 1.00 −05 7.31 −014.59 −04 3.50 +013.00 −03 3.50

774



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 1.00 −05 1.03 +008.97 −04 9.45 +012.00 −03 1.10 +024.00 1.216.00 1.251.00 −02 1.302.00 1.354.00 1.39

95 1.00 −05 1.03 +008.22 −04 8.62 +012.00 −03 1.00 +024.00 1.116.00 1.161.00 −02 1.212.00 1.255.00 1.30

205 1.00 −05 9.24 −017.32 −04 6.89 +011.00 −03 7.172.00 7.934.00 8.696.00 9.101.00 −02 9.652.00 1.02 +026.00 1.08

315 1.00 −05 9.24 −016.92 −04 6.47 +011.00 −03 6.762.00 7.454.00 8.076.00 8.411.00 −02 8.832.00 9.315.00 9.72

425 1.00 −05 8.62 −016.67 −04 5.95 +011.00 −03 6.262.00 6.874.00 7.456.00 7.721.00 −02 8.142.00 8.556.00 8.96

540 1.00 −05 8.62 −016.55 −04 5.81 +011.00 −03 6.092.00 6.624.00 7.106.00 7.451.00 −02 7.722.00 8.076.00 8.48



40 1.00 −05 9.58 −017.61 −04 7.45 +012.00 −03 8.276.00 9.241.00 −02 9.652.00 1.02 +024.00 1.05

95 1.00 −05 9.58 −016.87 −04 6.69 +012.00 −03 7.456.00 8.201.00 −02 8.482.00 8.895.00 9.10

205 1.00 −05 9.03 −016.35 −04 5.83 +012.00 −03 6.546.00 7.171.00 −02 7.382.00 7.653.00 7.79

425 to 540 1.00 −05 8.00 −015.76 −04 4.69 +012.00 −03 5.506.00 6.181.00 −02 6.412.00 6.633.00 6.755.00 6.85

775



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 2.00 −04 2.07 +014.00 4.148.00 6.213.00 −03 9.655.00 1.10 +021.00 −02 1.24

95 2.50 −04 2.48 +018.00 5.521.00 −03 6.895.00 9.651.00 −02 1.10 +022.50 1.17

205 4.00 −04 3.79 +015.00 4.48

205 2.00 −03 6.894.00 8.278.50 9.65

315 3.00 −04 2.76 +014.50 4.146.00 4.482.50 −03 6.832.00 −02 9.65

425 4.00 −04 3.45 +015.00 4.142.00 −03 6.213.00 6.897.00 8.271.50 −02 8.96



40 2.00 −04 1.93 +015.00 4.831.00 −03 6.413.00 8.271.00 −02 9.652.50 1.02 +02

95 2.00 −04 1.93 +015.00 4.831.00 −03 6.211.80 6.897.00 8.272.50 −02 8.96

205 2.30 −04 2.07 +015.00 4.488.00 5.521.50 −03 6.21

205 4.00 6.892.50 −02 7.79

425 2.50 −04 2.07 +015.00 4.146.00 5.031.20 −03 5.525.00 6.212.60 −02 6.62

650 6.00 −04 4.48 +012.00 −03 4.834.00 4.935.90 5.088.50 5.211.15 −02 5.361.70 5.583.00 5.76

776



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 2.00 −04 1.93 +018.00 8.141.00 −03 1.03 +022.00 1.106.00 1.244.00 −02 1.38

95 2.00 −04 1.93 +018.00 8.149.20 9.455.00 −03 1.10 +021.50 −02 1.174.00 1.24

205 2.50 −04 2.36 +015.00 4.83

205 8.50 8.274.00 −03 9.652.50 −02 1.10 +02

315 2.50 −04 2.36 +015.00 4.837.65 7.452.00 −03 8.271.00 −02 9.655.00 1.03 +02

540 2.70 −04 2.41 +017.00 6.211.50 −03 6.896.50 8.273.00 −02 8.96

777



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


TA

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-15

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FIG

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-15

Tem

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40°C

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re95

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Tem

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205°

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Tem

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315°

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425°

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.

778



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


TA

BL

EN

FN

-16

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LA

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FIG

.N

FN

-16

Tem

pera

ture

upto

40°C

,T

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ratu

re95

°C,

Tem

pera

ture

205°

C,

Tem

pera

ture

315°

C,

Tem

pera

ture

425°

C,

Ep

2.1

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Pa

Ep

2.1

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Pa

Ep

2.1

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113

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2

779



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 2.00 −04 2.07 +019.30 9.651.08 −03 1.10 +021.16 1.171.25 1.241.40 1.311.60 1.381.82 1.452.05 1.522.40 1.592.80 1.653.50 1.727.00 1.902.00 −02 2.071.00 −01 2.07

150 2.10 −04 2.07 +018.50 8.279.50 8.961.05 −03 9.651.25 1.03 +021.42 1.101.65 1.171.90 1.242.30 1.313.00 1.384.00 1.455.20 1.521.00 −02 1.594.00 1.658.00 1.681.00 −01 1.68

260 2.20 −04 2.07 +016.60 6.218.00 7.589.00 8.279.50 8.621.00 −03 8.961.12 9.311.25 9.651.39 1.00 +021.55 1.031.90 1.102.50 1.173.40 1.245.00 1.318.00 1.381.50 −02 1.451.00 −01 1.45

425 to 650 2.50 −04 2.07 +018.00 6.211.05 −03 7.581.25 8.271.35 8.621.48 8.961.63 9.311.80 9.652.00 1.00 +022.25 1.032.80 1.103.70 1.175.40 1.248.30 1.311.65 −02 1.383.00 1.411.00 −01 1.41

780



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


TA

BL

EN

FN

-18

TA

BU

LA

RV

AL

UE

SF

OR

FIG

.N

FN

-18

Tem

pera

ture

20°C

,T

empe

ratu

re95

°C,

Tem

pera

ture

175°

C,

Tem

pera

ture

260°

C,

Tem

pera

ture

345°

C,

Tem

pera

ture

425°

C,

Ep

2.0

�10

5M

Pa

Ep

2.0

�10

5M

Pa

Ep

1.9

�10

5M

Pa

Ep

1.9

�10

5M

Pa

Ep

1.8

�10

5M

Pa

Ep

1.8

�10

5M

Pa

B,

B,

B,

B,

B,

B,

AM

Pa

AM

Pa

AM

Pa

AM

Pa

AM

Pa

AM

Pa

0.00

0216

0.00

0220

0.00

0219

0.00

219

0.00

0218

0.00

0218

0.00

079

780.

0006

867

0.00

064

590.

0005

753

0.00

049

430.

0004

540

0.00

0879

0.00

0768

0.00

0761

0.00

0654

0.00

0544

0.00

0541

0.00

0980

0.00

0870

0.00

0863

0.00

0756

0.00

0646

0.00

0644

0.00

183

0.00

0972

0.00

0965

0.00

0858

0.00

0748

0.00

0746

0.00

1588

0.00

173

0.00

167

0.00

0959

0.00

0850

0.00

0848

0.00

295

0.00

1580

0.00

1572

0.00

161

0.00

0952

0.00

0950

0.00

2597

0.00

285

0.00

276

0.00

1562

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154

0.00

151

0.00

310

00.

0025

890.

0025

790.

002

700.

0015

590.

0015

550.

004

104

0.00

392

0.00

381

0.00

2571

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262

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258

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80.

004

960.

004

850.

003

730.

0025

640.

0025

610.

006

110

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599

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587

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476

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366

0.00

362

0.00

711

30.

006

101

0.00

688

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578

0.00

469

0.00

463

0.00

811

40.

007

103

0.00

790

0.00

679

0.00

571

0.00

566

0.00

911

40.

008

103

0.00

890

0.00

779

0.00

672

0.00

666

0.01

116

0.00

910

40.

009

910.

008

800.

007

720.

007

670.

015

118

0.01

105

0.01

920.

009

810.

008

730.

008

680.

0212

00.

015

106

0.01

593

0.01

810.

009

740.

009

680.

025

121

0.02

107

0.02

940.

015

830.

0174

0.01

69

0.03

121

0.02

510

80.

025

940.

0283

0.01

576

0.01

570

0.04

121

0.03

108

0.03

940.

025

840.

0276

0.02

700.

0512

10.

0410

80.

0495

0.03

850.

025

770.

025

710.

0612

10.

0510

80.

0595

0.04

860.

0377

0.03

720.

0712

10.

0610

80.

0695

0.05

870.

0479

0.04

72..

...

.0.

0710

80.

0795

0.06

870.

0579

0.05

72..

...

...

...

.0.

0895

0.07

870.

0679

0.06

72..

...

...

...

.0.

0995

0.08

87..

...

...

...

.

781



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---


TA

BL

EN

FN

-19

TA

BU

LA

RV

AL

UE

SF

OR

FIG

.N

FN

-19

Tem

pera

ture

20°C

,T

empe

ratu

re95

°C,

Tem

pera

ture

175°

C,

Tem

pera

ture

260°

C,

Tem

pera

ture

345°

C,

Tem

pera

ture

425°

C,

Ep

2.0

�10

5M

Pa

Ep

2.0

�10

5M

Pa

Ep

1.9

�10

5M

Pa

Ep

1.9

�10

5M

Pa

Ep

1.7

�10

5M

Pa

Ep

1.7

�10

5M

Pa

B,

B,

B,

B,

B,

B,

AM

Pa

AM

Pa

AM

Pa

AM

Pa

AM

Pa

AM

Pa

0.00

0220

0.00

0220

0.00

0219

0.00

0219

0.00

0217

0.00

0217

0.00

061

630.

0005

655

0.00

051

480.

0004

542

0.00

0434

0.00

037

320.

0007

650.

0006

560.

0006

500.

0005

430.

0005

380.

0004

330.

0008

670.

0007

590.

0007

530.

0006

460.

0006

400.

0005

35

0.00

0969

0.00

0860

0.00

0854

0.00

0748

0.00

0741

0.00

0636

0.00

171

0.00

0962

0.00

0956

0.00

0850

0.00

0843

0.00

0739

0.00

1578

0.00

163

0.00

157

0.00

0951

0.00

0944

0.00

0840

0.00

283

0.00

1569

0.00

1562

0.00

152

0.00

145

0.00

0941

0.00

2586

0.00

272

0.00

264

0.00

1555

0.00

1549

0.00

142

0.00

389

0.00

2576

0.00

2567

0.00

258

0.00

252

0.00

1546

0.00

492

0.00

378

0.00

369

0.00

2559

0.00

2554

0.00

249

0.00

595

0.00

481

0.00

471

0.00

361

0.00

355

0.00

2550

0.00

696

0.00

583

0.00

572

0.00

463

0.00

457

0.00

352

0.00

797

0.00

685

0.00

674

0.00

565

0.00

559

0.00

454

0.00

899

0.00

785

0.00

774

0.00

666

0.00

660

0.00

555

0.00

999

0.00

886

0.00

875

0.00

766

0.00

761

0.00

656

0.01

100

0.00

987

0.00

975

0.00

867

0.00

861

0.00

757

0.01

510

30.

0188

0.01

750.

009

680.

009

620.

008

580.

0210

30.

015

890.

015

770.

0168

0.01

620.

009

590.

025

103

0.02

910.

0279

0.01

569

0.01

563

0.01

59

0.03

104

0.02

592

0.02

579

0.02

700.

0266

0.01

560

0.04

104

0.03

920.

0379

0.02

570

0.02

566

0.02

610.

0510

40.

0492

0.04

790.

0370

0.03

660.

025

620.

0610

40.

0592

0.05

790.

0471

0.04

660.

0364

0.07

105

0.06

920.

0679

0.05

71..

...

.0.

0464

0.08

105

0.07

920.

0779

0.06

72..

...

...

...

...

...

.0.

0892

0.08

790.

0772

...

...

...

...

...

...

0.09

92..

...

.0.

0872

...

...

...

...

782



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 1.32 −04 1.38 +015.13 5.346.00 5.451.00 −03 6.213.00 8.204.00 8.695.00 9.106.00 9.387.00 9.658.00 9.799.00 9.931.00 −02 1.00 +021.50 1.032.00 1.03

205 1.43 −04 1.38 +015.54 5.346.00 5.451.00 −03 6.213.00 8.204.00 8.695.00 9.106.00 9.387.00 9.658.00 9.799.00 9.931.00 −02 1.00 +021.50 1.032.00 1.03



40 0.0002 210.0009 920.002 1080.003 1170.004 1220.005 1270.007 1320.009 1350.012 1380.1 138

95 0.0002 210.0009 920.002 1080.003 1170.004 1220.005 1270.1 127

205 0.0002 190.00095 940.002 1080.0025 1120.003 1140.004 1170.1 117

425 0.0002 170.00095 860.002 970.003 101

425 0.004 1020.005 1030.1 103

650 0.00025 210.001 830.002 940.003 990.004 1000.005 1010.1 101

730 0.00025 190.001 790.002 900.003 940.004 970.1 97

760 0.00025 190.001 780.1 78

790 0.00025 190.001 590.1 59

815 0.00025 190.001 420.1 42

783



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




40 6.80 −04 694.80 974.00 −03 1271.00 −02 1452.00 1543.00 159

150 7.50 −04 691.10 −03 992.00 1024.00 1121.00 −02 1252.00 1343.00 139

260 7.50 −04 691.00 −03 952.00 994.00 1071.00 −02 1182.00 1202.50 122

370 7.80 −04 691.00 −03 852.00 914.00 991.00 −02 1102.00 1193.00 124

784



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---




20 6.02 −05 6.89 +004.98 −04 5.70 +017.48 8.558.78 9.939.68 1.07 +021.11 −03 1.141.41 1.221.98 1.292.58 1.323.54 1.376.49 1.439.60 1.471.97 −02 1.545.00 1.591.00 −01 1.59

150 6.76 −05 6.89 +004.96 −04 5.05 +017.28 7.179.24 8.271.01 −03 8.621.13 8.961.28 9.311.48 9.583.22 1.09 +024.32 1.137.21 1.209.66 1.241.99 −02 1.335.00 1.361.00 −01 1.36

315 7.22 −05 6.89 +004.88 −04 4.65 +017.05 6.379.50 7.311.12 −03 7.721.20 7.861.30 8.001.40 8.142.51 8.894.97 9.657.10 1.01 +029.93 1.041.83 −02 1.105.00 1.121.00 −01 1.12

705 8.00 −05 6.89 +004.29 −04 3.70 +016.37 5.528.48 6.341.20 −03 7.241.26 7.311.35 7.451.45 7.522.88 8.624.43 8.965.73 9.317.49 9.511.95 −02 1.03 +025.00 1.081.00 −01 1.08

870 9.00 −05 6.89 +005.00 −04 3.83 +017.50 5.721.00 −03 6.651.11 6.831.11 6.861.11 6.891.11 6.891.13 6.891.16 6.961.20 7.031.28 7.173.28 8.274.79 −02 1.06 +021.00 −01 1.08

925 1.00 −04 6.89 +005.00 3.43 +017.10 4.897.50 5.127.80 5.368.10 5.588.50 5.828.80 6.031.08 −03 6.481.29 6.626.80 8.277.67 8.481.27 −02 8.964.82 1.03 +021.00 −01 1.08

785



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFT-1 2004 SECTION II

TABLE NFT-1TABULAR VALUES FOR FIG. NFT-1


40 1.00 −05 5.77 −011.16 −03 6.96 +011.50 8.202.00 9.722.50 1.10 +023.00 1.184.00 1.315.00 1.406.00 1.457.00 1.518.00 1.559.00 1.581.00 −02 1.601.50 1.692.00 1.712.50 1.741.00 −01 1.74

95 1.00 −05 5.00 −011.22 −03 6.27 +011.50 7.102.00 8.272.50 9.103.00 9.724.00 1.09 +025.00 1.196.00 1.257.00 1.298.00 1.329.00 1.341.00 −02 1.371.50 1.402.00 1.422.50 1.433.00 1.441.00 −01 1.44

205 1.00 −05 4.43 −017.88 −04 3.63 +019.00 3.961.00 −03 4.291.50 5.212.00 5.832.50 6.293.00 6.694.00 7.385.00 7.796.00 8.207.00 8.418.00 8.699.00 8.961.00 −02 9.101.26 9.451.00 −01 9.45

315 1.00 −05 3.92 −016.92 −04 2.80 +018.00 3.099.00 3.291.00 −03 3.461.50 4.052.00 4.462.50 4.773.00 5.024.00 5.345.00 5.607.00 5.929.00 6.141.00 −02 6.221.50 6.391.00 −01 6.39

786



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFT-2 PART D — PROPERTIES (METRIC) Table NFT-3



40 1.00 −05 5.67 −011.28 −03 7.58 +011.50 8.342.00 9.723.00 1.11 +025.00 1.238.00 1.301.00 −02 1.322.00 1.366.00 1.401.00 −01 1.40

95 1.00 −05 4.88 −011.23 −03 6.34 +011.50 7.032.00 7.794.00 9.247.00 1.02 +021.00 −02 1.072.00 1.124.00 1.161.00 −01 1.16

205 1.00 −05 4.42 −016.85 −04 3.14 +011.00 −03 4.002.00 4.964.00 6.146.00 6.839.00 7.451.00 −02 7.521.30 7.791.00 −01 7.79

315 1.00 −05 3.92 −016.85 −04 2.79 +018.00 3.091.00 −03 3.432.00 4.243.00 4.775.00 5.368.00 5.671.00 −02 5.911.50 6.071.80 6.231.00 −01 6.23


Temperature up to 40°C, Temperature 205°C, Temperature 315°C,E p 1.1 � 105 MPa E p 9.5 � 104 MPa E p 8.6 � 104 MPa

A B, MPa A B, MPa A B, MPa

1.00 −05 5.34 −01 1.00 −05 4.72 −01 1.00 −05 4.27 −011.19 −03 6.21 +01 7.33 −04 3.45 +01 4.40 −04 1.81 +012.50 6.89 2.00 −03 3.79 1.00 −03 1.995.50 7.58 4.00 3.99 1.50 2.071.10 −02 8.03 7.00 4.10 2.50 2.162.00 8.40 9.00 4.14 4.00 2.243.00 8.60 2.00 −02 4.22 7.00 2.314.00 8.83 3.00 4.24 1.00 −02 2.345.00 8.88 4.00 4.24 2.00 2.386.00 8.96 5.00 4.24 3.00 2.411.00 −01 9.10 1.00 −01 4.24 4.00 2.41. . . . . . . . . . . . 1.00 −01 2.41

787



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Table NFZ-1 2004 SECTION II Table NFZ-2

TABLE NFZ-1TABULAR VALUES FOR FIG. NFZ-1


40 1.00 −05 4.90 −011.08 −03 5.80 +012.00 6.964.00 8.146.00 8.831.00 −02 9.581.50 1.00 +02

150 1.00 −05 4.54 −016.72 −04 3.22 +011.00 −03 3.851.50 4.422.00 4.734.00 5.326.00 5.59

150 1.00 −02 5.832.00 6.114.00 6.28

260 1.00 −05 3.96 −013.83 −04 1.54 +011.00 −03 2.143.00 2.979.00 3.78

370 1.00 −05 3.48 −012.93 −04 1.05 +011.00 −03 1.483.00 1.999.00 2.59

TABLE NFZ-2TABULAR VALUES FOR FIG. NFZ-2

Temperature up to 40°C, Temperature 150°C, Temperature 260°C, Temperature 370°C,E p 1.0 � 105 MPa E p 8.6 � 104 MPa E p 7.5 � 104 MPa E p 6.4 � 104 MPa

A B, MPa A B, MPa A B, MPa A B, MPa

0.00002 1 0.00002 0.86 0.00002 0.75 0.00002 0.670.00289 145 0.00196 84 0.00151 57 0.00126 420.003 148 0.0025 85 0.002 66 0.0015 430.004 153 0.003 90 0.0025 68 0.002 460.005 157 0.004 94 0.003 70 0.0025 470.006 159 0.005 97 0.004 72 0.003 480.007 163 0.006 99 0.005 74 0.004 490.008 165 0.007 101 0.006 74 0.005 500.009 166 0.008 103 0.007 75 0.006 510.01 167 0.009 104 0.008 76 0.007 520.015 169 0.01 105 0.009 76 0.008 520.02 172 0.015 106 0.01 77 0.009 530.03 173 0.02 107 0.015 77 0.01 540.035 174 0.03 108 0.02 77 0.012 54. . . . . . 0.04 108 0.03 78 . . . . . .. . . . . . 0.045 109 0.04 78 . . . . . .. . . . . . . . . . . . 0.05 78 . . . . . .

788



--``,,`,,``,``,`,```````,``,`,-`-`,,`,,`,`,,`---

Documents

ASME SEC II D-M SB PT 3