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AD-A095 634 ROCKWELL INTERNATIONAL DALLAS TEX COLLINS RADIO GROUP FIG 17 STRESS ANALYSIS OF AIRCRAFT MODIFICATIONS IC-INIB AIRCRAFT). JO--ETCIU) OCT 80 D 8 RAGAN F09603-RI-C-0602 UNCL7ASSIFIED NL 2flflfflflII lflfflIII IIIIIIIIIIIIIIl.... EEEIIEEEEEEEEE EEEEEEEEEEIIII EIIIEIIEIhElIE IEEEIhhIII

ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

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Page 1: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

AD-A095 634 ROCKWELL INTERNATIONAL DALLAS TEX COLLINS RADIO GROUP FIG 17STRESS ANALYSIS OF AIRCRAFT MODIFICATIONS IC-INIB AIRCRAFT). JO--ETCIU)OCT 80 D 8 RAGAN F09603-RI-C-0602

UNCL7ASSIFIED NL2flflfflflII lflfflIII

IIIIIIIIIIIIIIl....EEEIIEEEEEEEEEEEEEEEEEEEIIIIEIIIEIIEIhElIEIEEEIhhIII

Page 2: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

I RE VIS,

LTRJ DESCRIPTION DATE APVD

IV I I/

STESANALYSIS -

OF-

AIRCRAFT MODIFICATIONS 2 '.92

(C-141B AIRCRAFT),

~JOINT AIRBORNE OMMUNICATIONS NTER/COMMANDPS

(JACC/CP) PROVISIONS

EMIL :.-IV1

- - - - -Approved for public release;im~l iL 1224127Diethb-buion

Unaimited

97 989910( 101102103 0 410o510 06 0 81 10 io11 11131141511(117118 1912(

73 r41516 7 77180~ 8~ ~ 8 8 90992 59

49 50151152 53 5455156 57 55960 61 6263 4 65 6 76 6 07

25L2627128 29 30 3132 3334 35 36J -8 9 0 4 45146147ATSIRV------- - - mm.IA I~A

OFSH SIHEE 1 23 567 811 12 1314 156 17 92 12 23-24CONTRACT N .ROCKWELL INTERNATIONAL CORPORATION

/~Fd9663-80-C-0602 COLLINS RADIO GROUP

PRE &0B N ~48 DALLAS. TEX 75207 NEWPORT BEACH, CALIF 92663 CEDAR RAPIDS IA 52406

STRESS ANALYSIS C-141B AIRCRAFT_________________ JACC/CP PROGRAM

A PVD lo/A -J' SIZ CODE IDENT DWG NO. rN

A 134991 649-2924-001 -METRIC

_________________ SCALE IsH E 1 OF 127

A REV- TIC CR __NE ri

Page 3: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

REVISIONS

LRDESCRIPTION DATE] APVD

STRESS ANALYSISOF

AIRCRAFT MODIFICATIONS

(C-i 41B AIRCRAFT)

JOINT AIRBORNE COMMUNICATIONS CENTER/COMMAND POST

(JACC/CP) PROVISIONS J -

lif

QF SHE jSIHEET 1 3 14 15 16 17 18 19 11011112113114115 116 117 118 1191120 r21122 224CONTRACT NO. ROCKWELL INTERNATIONAL CORPORATIONF09603-80-C-0602 COLLINS RADIO GROUP

PREP .B. RGA? 024-80 DALLAS. TEX 75207 NEWPORT BEACH4, CALIF 92663 CEDAR RAPIDS. IA 52406

CHK STRESS ANALYSIS C-141B AIRCRAFT__________________________JACC/CP PROGRAM

APVDSIZE CODE IDENT DWG NO.

A 1 499649-2924-001 METRIC_________________SCALE IISHEET 1 OF 127

REL REV- TC__ CRNBDL_ Ti-

Page 4: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

TABLE OF CONTENTS

SUNHARY

REFERENCES

1.0 AT1108 UHF/VHF/AM ANTENNA INSTALLATION P. 5

2.0 H.F. LONGWIRE INSTALLATION P. 9

3.0 UPS-192 HF RECEIVE ANTENNA INSTALLATION P. 29

4.0 437S-IC VHF/FM ANTENNA INSTALLATION p. 32

5.0 DMC34-3/B UHF SATCOM ANTENNA INSTALLATION p. 47

SIZ C O DE__W E NT______N O._649 -2924 -001_

Page 5: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

SUMMAkRY

Stress Analyses were performed on the following aircraft modifications:

* ATl108 Antenna Installation,

. HF Longwlre Installation,

* UPS-192 Antenna Installation,

* 437S-1C Antenna Installation/

* SATCOM Antenna Installation

The detailed conclusions of each of the topics above are contained after each

sub-analysis. However, the general conclusion is that each of the subject modi-

fications in no way impare the airworthiness of the aircraft in that the aircraft

strength is equal to or greater than the original unmodified strength.

I.I

: _SIZE CODE IDENT DWG NO.) ~~~A 13 4 9 91 , -SCALE IREV ISHEET 3

Page 6: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

REFERENCES

1. T.O. 1C-141A-3

2. NIL HDBK 5C

3. Formulas For Stress and Strain, 5th Edition, Roark & Young

4. Analysis and Design of Flight Vehicle Structures, 2nd'Edition, E.F. Bruhn

SIZE CODE IDENT DWG NO.

A 13499 649-2924-001

SCALE REV SHEET 4

Page 7: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

~ Mo. 6P4-28e3-ooi

The a,7 en 15 mqotfec on toe of -the. fu,,Se/e

COOsS1r of a. Yreav-anevla/r pA7'e 5.1/Z X~ 17.Z&S)K 07-3

ahk f/ht c ea -to 7%e or~y iai/ s kin a Piv/ a 7 ?

6.9 0x .*08 0#-1A* c/oc, /er,' -r/,e -n~ Ytivers Ore

AMIS 10?7 D 4 7-4e pe~ <re trwo0 .7-5-o D14, holes ih

dcu(er 4wlo Filler platde.

149- 28 77 I)OCAb/er

( S -5t t-4 oforic/~Sn S2 *fr'c*~re.

,sk7Y7: -70 75 7- C/1sc/ OcS-K t74* (f

Crjtt~cta 6hier bwuck/itig cff-res-sfOe'e

ct: 2oo 3 3665

5 ~ Ie 3 ft(e .3 ,e-n7, 4 L

- *385 Psi!

ISIZE ICODE IDENT IDWG NO.A 1134991 649-2924-001SALE IREV ISHEET 5

Page 8: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Cri+IC4/ 6k'e-r f/ 0o-i /,47

,7- r .L

-8551 (.06>" 4 79 /'/47

(b) s -renV-4 oF Fi/er , e : oZ4 r.3 .0 3 t-,4k-.

Scr /"" " 9 IV 12 i7

Cr,+lcaI 5(.ier FIo,a

%C r , - 3 9j 979 (.o 9-3) -343 ///,

SfrejAf o4: d/o uler 0Z 4T3 .08 o 4 T-.

CZ 7. = ,

"6 6.?o = /.-

I 12.7

Q. 7 ( 1 1 o/ PSE:E

SIZE CODE IDENT DWG NO.

ALE IREV ISHEET 6

-soon-.

Page 9: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

(c) C,rcu/l'r CLJ7o(4"

A4g- , 'e areeA be71-weevp ceej ope 7ffec-*,vp

V- V2.-- z ( - .- s s

, -e .IT 2(.o8) 1(. - 5.5y 8 AVoM , = 3. ~ 7, 7)( 1,q) = 1 I8 Al- ,'A." '

Thbls 1n f&;n 15 re4 et r 71~,'C o#71J Wen CoS~ rvj -He C, rec e'ef fje",, e 47'' e r

-two Actes wff oic 'ast/ rf s'-r bei0/,,9

mA i. um 13 e -54 , Sr e -

188 , -3o5g

6~ s~2.024 73 (Ref 2

4 64000 /---.9/\, ,33f

SIZE CODE IDENT DWG NO.

A 1134991 649-2924-001ALE REV TSHEET 7

Page 10: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

T (a' C OA.'sI DhR PU SLF T-,6AJ/oMA 1-04D 1AJ ,1y~

Lo aot /0.5 -t~ CU-tOUT 1)7 S/'fr

72Z000P-Si (7S )(.6 J 3024 /bs

U5r7 P;/e as lo c/ Ca rry f v 07e#"6er

2O2.# 7'-; Fil- z Z ksi Re,,.. - (zRef 2)

M .1 -+7)(0T1

Use AS /oc?7,D4 r,/et-s -1o -fr4,3.sF-r /cal 0A //d'7

rvet- 44 4

riVe t-, r rn~/ed = Z30

MrIvS', - -l -lZ

(e) rrcr

7c12re ire 07e 4 cc etS' AI. 1. /51

*I-,e *"nI/ Inloc e lc ls 4 the f/ c~'~~l' i 7 -j

$H71e cv4y-A

MGIS (Teost'/c ct

SIZE CODE IDENT JDWG NO.

A 134 991 649-2924-001SCALE IREV --- SHEET 8

Page 11: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

2-D H.F. LONGWIPR? .TN\ST/1LL/TO

Twvo HF. Io#7,wie c4flen4,s ctre murrtec o-n theuepersl, e of~ -t-he aircrnfr eTr Fs Izt, L. " R 1

44.56 j W.L, 27~ awdic Con necle/l *o- -//e k

tr vc u 'rue t c4i' If r P~c po'it c FSK.

L i3L 8.0 WL4570

RPef-re nc e- D ra w~n~s: 64l 84 nsIat

SIZE CODE IDENT DWG NO.A 13499649-2924-001SCALE IREVSHE 9

Page 12: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

6)eo met f~vFjh+c/k/

FS 951

(~8.0Wr L 45.2.

1BL 44.56WL 45o. Z/

. "- "- -k?.0os"

C (F-s 1126.1 IzF, 1 5. /8L 44. 5$ L 14.56

272.32 WL 272.32

51-0- 1 177.89 _ 17,3 °6b-f Z/

7. .3,3

)177.8 -7 17. 3305'17.33

I SIZE CODE IDENT DWG NO.

1134 991 649-2924-001

SCALE (REV (SHEET 10

Page 13: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Verticed Sc4 6 1I4er Iaiercx/ rnveme),I'

-- WL 540

24(14 2 -2-) WL 450.21

14. 232 \ ___WL 308

X 147/ lnvcles

0, ~34_.1 -F 14-7/

Ten/on7 -f-oke up m Us-r mi ve J-,6 4 5177. 33 08~ ~4

SIZE CODE IDENT DWG NO.

A 134991 649-2924-001

SCALE _REV ISHEET 11

Page 14: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Load on fadlFli'

Pr.,,,,,: Tenso, x So), c, ,,,= 10.5 7 Ih

-,Te b

56.r Tensin C e' c* 13)

=IZ74 i4s

L w Ire,

lrc&kinj STre if C+

wire bCI

STen ion = 850 , 1/'- )1 75-

* J,,L 0 ( = .3,52 (rc

4/0I I

II

A 1349 649-2924-001

SCALE IREV ISHEET 12

........

Page 15: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

b) YFai/ Fi#,nf y P14' 649-2t8oJ

Ma-f'L 20&4-T351 QQfi2,Z5O/4

Fj 6zooo Pse' (Ref 2)

3 O00 PSI' a00

Fl II5 ooo s c' (e/Dp)

Bea~r i-n Fccto r 2.0

~e~r~Filti)j5 7Fe~c-rr 1.15

1L 7 25 ) - 5/Oo 00 se

JI5oo /5/-ooo 2

SheCr e C ro(

Z (-/0) (S- 0.2-Cos 4o-) 20

t(./' /;, iS ecured/ -f6 */,e #o,/isruc'turc-',/-&I/?5 5 /7- 4 blft5 /u/0ooo As 1'/7 m17;pun'U Trs,

the 4tcooi're 15 secc.jrel -to the fiym C'c'

141,14 bol-. 3% IeCs-trei- 7(/ of 3K 1&s.SIZE CODE IDENT DWG NO.A 134991 649-2924-001

SCALE IREV ISHEET 13

Page 16: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

C) Th-ternnet /fa.5-- ;7s t4A//e-?L o P/Av/ 6 I 83o441

F51126o.12 MS 24 69 3 5cr ,.,, ( 6)

p.W" EXISTING STRINGER

__ R8L 47.093LSL 42.037

oRBL 44. 5/5105"" I-"- __ -_1274 1 M,4. 6

AIRCRAFT SKIN

RSL 42.037LBL 47.093

- tTEXISTING STRINGER

/1 2.50 /,c c/aleter lioe /,s Ct' L,; , -fe c;7 ~i -the

For" the m cts /,7 S-fel 7 0/ ,.

5)i 70-- -' 7-/C-/a d 0 5 Z -N1 (Pef

Ft -72oo ps " (ze f? Z)

P 0.5 56)(720 00) /o 080i/s.

7T O c/ oule/rz c~re used "to carry /oac/ -/'bt p/u.s

J/i-r6U-e "-ib /Z74- lb iL.'nrwire /coc i .) 7,'<r

skZ 6 c ic/ l*re)er.r

Re-F. dro ,v) s 649- 2638 Jcc.,A/e

649- Z83e c/oubler

SIZE CODE IDENT DWG NO.

A 1 134991 649-2924-001

SCALE IREV ISHEET 14_ __ _

Page 17: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Doubl/er Plaerl2/l Z07Z4 - 73 ~~~~

ft 6e)O 00pSL (k'ef Z)

EXISTING STRlilGER A

OL 4ZZ 7 - - - . - =-q7D4

RDL 4#-%S + S - --41 +a +

-~49-ae37-, AA~ fr.~ C(RAF

M5.~~J4 /0, Cje-17

~?1FS Cc1261126(I'o N~ q ~ s 197 (22 .5o5 /v7 D NA-5 1097 D (m4

/0., 6,560 + 27

14 4 4 IL

1SIZEj CODE IDENT I DWG No. 6922-0A 13499 64-9401

PSCALE IREV SET 1

Page 18: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

M5s 1444o _______ .27

1/35-4

3.7

S~e~r ic~c~2 274 C cx5 /7, 3' /?6/~

/c~~c-~ ((d' /274 ,'j ,7 )b

L 6 c C'T r,~/

j?/6(IC37f (1.875)- 75AC

zF 7-32 k

~74 // /6S~ er ,)- vi S 2 46e2

SIZE CODE IDENT DWG NO.

Page 19: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Rna~j~sOf 4V7/e. 647- Z83c

AD 1 /134- IZ04 78-

TX -0/24 -239/.-3----I

A 13

1&4.5 //,/, , I1,s.

o/zP/

C--/5840 PSI M. +

FIZE CODE IDENT DWG NO.

SCALE 6REV SHEET 17

Page 20: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

)Coupler rnoun-t 6qI-Zo

gv~~c*fT ~gi

- IP

CO UPL FR

Fwd

SAF-r

clip 61- l

CCLI

SIZE CODE IDENT IDWG NO. 6922-0A 113499 6922-0

SALE TRE V ISHEET 1

Page 21: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Dest g2 /oAels per NIL-A-8865

F d . q 9. 8 4I F T. /-5 3 F- 15.7 , -e.e4VerT-. 2.0.3 up

Lafer4. 5 clo

Ultniate /ococ/s exre /.9- des(r

Loadc CI,,srLyut/or, o- FP=7Vertic&/ supports 14.7

25.56VFw''cl s upr' 14.745V8C I IL,"

2 9 .-- I ) -7 7 L .6

F~ .45 V

7_.MA = .55 ('37)(a4..sz)(.7.5)-/ 77908,v-t

19 / 85 /5-.

A 13,499 6492924-001-

SCALE REV 'SHEET 9

S9. .-5 -) -/ Z 7

Page 22: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

sec/Or7 protperfi o a-f ubo/etr sueort' s~tufs

A-rc 4. . /58 l~l

K I = OOC758 ,V4

5Stress c47f doinif C ori hori~onf-a/ fr,

-- q07' (.37S) 35o ps

Mva ,LL eropertleJ e0o24 7-3 t-bIn9

F 6 4000 p,5' (eF2

M5 -3500c~ Shear 33.

SIZE ICODE IDENT JDWG NO.

A 134991 649-2924-001

SCALE IREV -SHEET 2

Page 23: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

1__ 64o±. 22 8T7

fta-L.9. Z024r

INFIPP ~14O E fP

A i. 2 5,4 PL

DIM4. B

6n lo 4 kse' (e/ci/.5

7WSe), CCrcs $ec?'#&i 4

= 038 1 ,AL

Z( 9572o1S M~0038

476 Sc AA S +

ISIZE CODE IDENT I DWG NO.A 1134991 649-2924-001

SCALE IREV j--SHEET 21

Page 24: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

c/.3) Lo ac/ -n cz F-r Vert cd S'a -r ri Ver p/tTerA

VIA

I./:S S70 -7-

' ', I

\\ \

- --- 4- ~ -u

Z Z~~~~~~~~~ 2 7". 3 ,,, 9 / < S3o e/- .

M.D. +

'p 4

SA ecr r =2/ 2/1 &

SIZE CODE IDENT DWG NO.

A 13499 649-2924-001

SCALE T ~ ISHEET 22j

Page 25: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

p~ M20 IP14/- reachWl /.1o ible C?/re rafi /

6ki" by 2 A4S 10171W6' rivers Pv(707 1/.5 : t~'f3yle .54hear ec~c/) a via/P1

W15 &/0,7I 7D5 r''e'rs (olls 1 sSlh!3/e 5 ear)

cad! pe r r ivet q 97 14 19 M3S +

5-.-77

TA/j /oae-/,s -IreinsFe.re~/ b3 2 tv1SO47011J)4 rIlVe-r5

EXC#" rC /OCAC(On rlve' A4 ~

.6 (=)(3 1:33 452- (. 3 1)Z o0 a4

Shear 5-t-renIt4 o'f MS Zo047o/Il4 u,toc 06-3 9tL/-5 3 88 /.s C(re f a)

m4 3.3 6 ___ _ .84

ISIZE ICODE IDENT IDWG NO. 6922 -0-A 1 13499I 6922-0

SCALE IREV ISHEET 23

Page 26: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

J.) AtnLY-3,s oF DR,9G 13 RPc S'YsreM

MIS E7039-1 cl/iPe~44 -Z82Z c/,c B

pp

,, - .41

649--a I

rwvc/ loaid 37(clg)(,5)

,4xl~y4 Z0,1 /I /R961 s 4cz

50c.5

=P0 57245Co.5 C

- 572 34 03 pAs .5. +•1 8

P -5-oc Ti 2-e' a° 77 1,.5

p- 277 55 16/b/± M45 -

SIZE CODE IDENT IDWG NO.

A 1134 991 6-29 -°T24SCALE IREV SHE 24

Page 27: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

,. s,, - clIecp ,4- MZ *6~-2

A3ssume al/ 5oo 1b load .oes AJD 10/3,4- 1003

Into the top +wo M$?7o3'-I I -i-'°h

~saumC a 5ec+/'on .38 w"nchesw de o?7 ecc( 5ide of Fastener .063 Re-E I5

esls-ts load L.7I R5du7

" -75(.87) _1ec+iV'e A't-/

50 0- 25o (.o)(.o?.3) _&2755s psi" 5- l

0)O Xio4 55-Ps

M -'L 65-re-7hA 'or 2c24 -T3-// e xrP./ck

P 5'1 coo pse liT (R~ef e)

Ps 540 oo _s,(/ _____ _____ 13

? Z 75-5--

Fs 2-00

.o(3(.4o) # ~

6 eo 108000 tr~'o, (e/

000 25o 2c2 p.s i 1

2r7- 4 12_____

g./ 7) 2-63

SIZE CODE IDENT DWG NO.A 134991 649-2924-001

SCALE REV SHEET 25

Page 28: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Ioqf- T Draff /0c I Carr;e I Ico 7It P 5g .,MRS 1097 P, rivers -ad 5., N115 1097DS -f-e~

,8 I El 5? r---4,II f -.. o I . I

-F--i, '..I_ T I IA1: I

±ilT T' i1I - .50-

VIEW C-C

7-rfc,4 YSc~ 5-rr6e 5. v IVe 7-s

2-6 56 Psc'

e-1

2(.~e#-f~c~t33 II L

-- 6r -SI-f Z* r V'e 7'

-,1 -- 331 5 -72- psi i's. -5-

A 1349916924-0

Page 29: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Ceirr,*ed by -t~e 647-Z2812 C'c4flneI -to #h~e cvrof-,S-Fr *76ers ±tA r t rh e 64 -7- Z // /i~ s, tA e c/ p3 a reSecuc.red -1o -the Sir-Inyers by P-- Alls 2 e47o /1-P4 r I'es.

VerriCed load' -t tl rjrv5,zS

V~ 77cos 32 ~ 37 /bsq'fV PV, 2 77 !bj

Shear locWc t-o Ski..

5 t ik-o r 8z ihA.. ±A-e ~ra rICOc! Clue #o o-clcea 1

Vev-fI6J /1c0c-( Str ~ S,7 (2z37) = 14o0 /ks

~Eicev-+cic /celacYC riv'ets

lp / /,/-(10 .

i~/ ~/ /0 -70 /

13 3E E, 2)

SIZE CODE IDENT DWG NO.A 134 991 649-2924-001

SCALE IREV ISHEET 27

Page 30: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

te H COwI0,00e Of +4 ven-cc1 loear/ .s 113 aswklc* /s sheearec/ in/- 'the -sk, 7, rivers

$#ress op-, riVet5 1 4-3 9 q'7 i'st

LooelOv) iver 3 2- (. oz8) .- (,'o

Th Ye5uI+fent 5r-ces-5 ()j7 -l ve-l 6 (r'r, 5tre~ss-elriver)

R $148 Psi e'747 tO3' -W-Rie

Wl/owej,/e .54 eezr St~ess o.i 201'7--73l 5872 P-e'

(-D) riV~r- is 34 00 o P'-SI/ ~ N

PIS__ ____ 1__ _00 4,,72

5~ 9 4g

The '1'~fsJ /c~s-t/--t t4c c/eigl 15 of 5/f//~

7ej~ o carryf all! Ine/uecl/ 1/coliS (u /#Y47-1ic

/-ek7/o OB(P. ?0o)SeN11n 0 O/ (P.-3)

rivet OfteC4fP7 IMS =0. 27 (P. fill

SIZE CODE IDENT DWG NO.

A] 1 34991 649-2924-001

SCALE REV ISHEET 28

Page 31: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

~3.0 UPS-192? H.P. 1?ECEIVE AN N~A TNSTL

DWG. NO. 64-9-2797-00/

The atY77enna~ is nfd7+aunec/ o,-, +/?C bolto# 7 O-f

-the 4Quse/ayje 0cd- F.5- 8 46, L 13L 2. 95. TALemc/;,f1ccdf on Con st roc-F ct oc,6 /er 4.2Z5 "xO..oo "' K

.080 tk. a7'7'-ac e- '% *Ae ns/e o f t 4c F(.s/a1

5k by 34 (VS /0-77 P 5 rivets. -the Is oie.

.,906 dl::nw/eer ho,/e c/r,'//ec/ o7 l' cenIer o-f +he

clo &i k le r

Re efe rc ) e Tra w.'nS 4c - 79c?7 -Tn s//~v

e4- 4 ,, Doub/lerJ

C Co >7s /e r C cn- pr ec#- /csc O n .5c 7-0 n 7 5sk4

Lcoc /C~ b~ cftoul- In 5klrn

5 k'nis 70 77 7-,/ C/ac! .7/ 7-AX\- (ReF)

Lcee/ ocjd/iycf cr'A/cr

tnaYoL 2024 T,3 .0c>~ jhk.

3c" CO o P

Rp~6 ,~ 3?'o 0o ( 4 . 0efr 2 -3 2~( c) 8 550 /b.5

1,llS. 8 8552 _ _ 4-5ISIZE I COIDE IDENT IDWG NO. 6922 -0A 134991 6922-0

SCALE IREV ISHEET 29

Page 32: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

(b) 13uckI/6,P7o? ef 5e Y

Cr;-'h/ buc//in sress of oreIn4l e.,'rcrol (- po e

-For b - k 5.5 (eef 4 PC5..3).07/

/0r I, 330 psZ

bw 4.Z4 - 08 t . 080

b : 75- - 0 : .-7 1 web

k L 4 . 16 (Ref 4- P C6.3)

_ 77- E / 1s

, -84- , 2sC

13 203

SIZE CODE IDENT DWG NO.

A 13499 649-2924-001

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5eCf/o1 Pro pert /es of a -- 7/e 715tof -e IoIm

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Reacion5 oni an3/c K49-289?-oo/ (worsTr Cc4se)

-- 'ANGLE-' -ANTENNA ATTACHMENT.----..... .. .

* ICES STRU[L-II THE STRUCTURAL DESIGN LANGUAGE

* CIVIL ENGINEERING SYSTEMS LABORATORY ** MASSAC4IUSEITS INSTITUTE OF TECHNULOGY

---------..----- CAJAHAIDGEt MASSACHUSETTS

* 14.24*47 09 OCT 80

* UNIJIVAC 1100 SERIES EXEC 8 ** VERSION 2.7 *

PREPAKED BY HAARTEN VEY

iOJE COOKOINATES

x Y

1 O.Oj D.Ou SUPPORT2 1,0'1 0.00

3 '4.74 0.00'4 5.7e D."1u5 5,8? ).00 SUPPORT

T Y -'E PLAAE FRAME

1 112 33 t4

'4 5

"AEr 1 £R Pqf)PLHTIE%

1 I4 19 Sb fis65 I U326 SZ .P326

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SCA7LE , - REV ISHEET 37

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F-CON~STA'NTS--------

-Et - 19UOE7 -ALL---.

G 3*dOE6 ALL

LOADING - 't)AG'

NODE - LOAOS

2 FORCE Y +90.6- FORCE Y +21.' 4-

4 FORCE Y -544*8

STIFF14LSS ANALYSIS

UNIITS KIPS

OJTPUT DECIV4AL 4

LIST FOr-CES.NEACTIO'jS, DISP'LItCEP.CNTS ALL

OJTPUI DECI?'AL 3

LIST 14AX STRESS,EACti LOA09ALL MLMBERSSECT FR DS 0.00 0.20

1SIZE 1 CODE 4 IDN DWG NO.

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SCALE IREV [SHEET 44

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Page 49: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

5. 0 .5TCOM ANTENNA TINSTALLATION

DVVG. No 649- 295)

CALE IREV SHEET 47

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SCALE IREV ISHEET 48

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SCALE IREV SHEET 49

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Te so n Oal cylb,'/J /0-57 b r CurCLJ'7

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f//& (. W-q) = 3 c,14s

r rive tz cor e uc,'sc/o ven *m Sre 'trj

( 3 -= / ___ c16s

Page 53: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

SUMMARY

AN ANALYSIS WAS PERFORMED ON THE HONEYCOMBY AIRCRAFT PANEL, P/N 3W12010, TO

DETERMINE ITS CAPABILITY TO REACT THE FORCES INDUCED INTO IT BY THE UHF

ANTENNA DUE TO AERODYNAMIC LOADING. AS THE ANALYSIS PROGRESSED, IT WAS

DETERMINED THAT THE ANTENNA SHOULD HAVE A ZERO ANGLE OF ATTACK, RATHER THAN

THE 7-DEGREES USED IN THE ANALYSIS: THUS, THE ANALYSIS IS SOMEWHAT TRUNCATED.

HOWEVER, THE ANALYSIS DID SHOW THAT THE PANEL IS MORE THAN ADEQUATE TO TAKE

OUT THE SHEAR AND BENDING LOADS INDUCED BY THE ANTENNA.

SIZE CODE IDENT DWG NO.

A 134991 649-2924-001

SCALE IREV ISHEET 51

- "

Page 54: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

1.0 ANALYTICAL MODEL

AN ANALYTICAL MODEL WILL BE MADE OF THE HONEYCOMB AIRCRAFT PANEL

TO WHICH THE ANTENNA ATTACHES (SEE LAYOUT THAT FOLLOWS). THE

PANEL WILL BE MODELED USING TRIANGULAR FLAT-PLATE ELEMENTS HAVING

BOTH SHEAR AND BENDING CAPABILITY. THE ANTENNA WAS ASSUMED TO BE

ATTACHED DIRECTLY TO THE AIRCRAFT PANEL WITH THROUGH-BOLT INSERTS

IMPLANTED BETWEEN THE HONEYCOMB FACINGS AT EACH ATTACHMENT LOCA-

TIONS. IT SHOULD BE NOTED THAT IN THIS ATTACHMENT CONFIGURATION,

THE ANTENNA HAS A NORMAL ANGLE OF ATTACK OF 7-DEGREES.

BECAUSE THE STRUCTURAL CONPUTER CODE USED IN THE ANALYSIS DOES

NOT HAVE A HONEYCOMB FINITE ELEMENT IN ITS LIBRARY, AN OVERLAY

ELEMENT WAS FABRICATED FOR THIS PURPOSE WITH THE TRUE SHEAR

THICKNESS AND AN ARTIFICIAL FLEXURAL MODULUS SO AS TO YIELD THE

CORRECT FLEXURAL STIFFNESS.

SIZE CODE IDENT DG NO.A 13 A-1 99 64-92-0SCALE IREV ISHEET 52

074-8679-140

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tSOO -. 0

.99

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) -- 4. . .. ...... .. - . ..... ( 1.6 /tr9

.. .. .. .. ... I .. .....18 #

0 0 , , 0 0 , 0 0

SIZE CoD iDE- --(WG NO. - ..

SCALE IREV IHF

Page 56: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

'C1l1-B' "OM C34-3/B UHF ANTENNA MOD'

* ICES STRUDL-II *f I THE STRUCTURAL DESIGN LANGUAGE

* CIVIL ENGINEERING SYSTEMS LABORATORY ** MASSACHUSETTS INSTITUTE OF TECHNOLOGY* CAMBRIDGEt MASSACHUSETTS

* 08.18,46 30 JUL 80 ** *

* UNIVAC 1100 SERIES EXEC 8 *• . VERSION 2,7 ** *

PREPARED BY MAARTEN VET

NODE COORDINATES

X Y z

1 32.60 638.50 239.702 32.60 641.27 290.593 32.60 644.04 291,484 32.60 646980 293.375 32.60 649.57 293.266 32.60 652.34 294.147 32.60 655.11 295.038 32.60 657.87 295.929 32.60 660.64 296.8110 32.60 663.41 297*7011 32.60 666.23 298.1612 329bO 669.05 298,6213 32.60 671.86 299.0814 32.60 674.68 299.5415 32,60 677.50 300,0016 10.b0 638.50 295.0OO17 10.50 641.27 20,5.3618 10.50 644.04 295.7119 10.50 646.80 296.0720 10.50 649.57 296,4221 10.toO 652.34 296.7822 10.o0 655.11 297.1323 10.o0 657.87 297.4924 10.50 660.64 297.8425 10.00 663.41 290,2026 10.o0 666.23 296.56 ......._---

27 10.50 669,05 293,92 SI Z E CODE IDENT DWG NO.28 10ob0 671.86 299.20 13

S 4 649-2924-001SCALE EV 1 H E .

Page 57: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

SIz

24'S x1L Se /+--- -F £8

- __ __ -' a* ZSt7L -. 95

7is $;Q~ LoS, 6.k

~ 0 0 9

14) 4.

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S- - . .v---

29 10.50 674.68 299.6430 10.50 677.50 300.0031 13.00 638.50 294.9532 15.50 638,50 294.9033 18.00 638.50 294.7034 20.50 638.50 294.5035 23.00 638.50 294.1036 25ob0 638.50 293.7037 28.00 638.50 292.7538 30obO 638.50 291.8039 13.00 663.41 298.2040 15o,0 663.41 298.2041 18.00 663.41 298.2042 20.50 663.41 298,1543 23.00 663.41 298.1044 25.50 663.41 298.0045 28.00 663.41 297.9046 30.b0 663.41 297.8047 13.00 677.50 300.00

48 15.b0 677.50 300.0049 18.00 677.50 300.0050 20.50 677,50 300.0051 23.0 677.50 30090052 25.50 677,50 300.0053 k8.00 677.50 00o.0054 30.50 67750 300,0055 13,00 644.04 295,6756 18.00 64,Ot 295.4857 23.00 644.04 294,9958 26.00 644,04 293.9259 13.00 649.57 296.3960 18.00 649.57 296e2661. 23.00 649.57 295.8862 28.00 649.57 295.0863 23.00 655.11 296.7764 28.00 655.11 296.2565 23.00 660.64 297.6666 28.U0 660.64 297.4267 23,00 666923 298.8668 280,U0 666,23 298.3269 23.0 671.86 299.6270 28900 671.86 299,1671 15.U7 654C.00 296.7072 17.69 654.00 297.0373 13.15 656.06 296,88T4 19,00 656.06 297.0375 13.75 658o74 297.40

76 19.00 65i.74 297.4277 13.75 661.41 297.94

78 19.00 661.41 297,9279 13.75 665,41 298.5180 19.00 665.41 298.5181 13,75 667.89 298.9062 19.00 667.89 298.9003 15.75 670.37 29929 SIZE CODE IDENT DWG NO.84 13.0 670.57 299.6 2 1 9 6 9- 1, F96T2.5j f.6 % Ql 649-2924-001

SCALE -- Ve 56. HEf..

Page 59: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

86 19900 672.56 299.6387 15.07 674992 300.0088 17.69 674.92 300.O

101 32.60 630.50 289.50 SUPPORT102 32.60 641.27 290.03 SUPPORT103 32.60 64,04 290t98 .UPPORT104 32.60 646.80 292.87 Si:PPORT105 32,60 649.57 292.76 SUPPORT106 32.60 652.34 293.64 SUPPORT107 32.60 655.11 294.53 SUPPORTlot 32.b0 657.87 295.42 SUPPOKT109 32,60 660.64 296.31 SUPPORT110 32,60 663.41 297.20 SUPPORT111 32.60 666.23 297.61 SUPPORT112 32.60 669.05 298,12 SUPPOV113 32060 671o86 298o58 SUPPORT114 32.60 674.68 299.0o4 SOPPORT115 32.60 677.50 299.50 SUPPORT116 10.50 638.50 294.50 SUPPORT11? 10.50 641927 294.86 SUPPORT118 10.50 644.04 295.21 SUPPORT119 10.50 646.80 295.57 SUPPORT120 10.50 649.57 295s72 SUPPORT121 lobO 652.34 296o28 SUPPORT122 10.o0 655.11 296.63 SUPPORT123 10b00 657.87 296.99 SUPPORT124 10.50 660.64 297.34 SUPPORT125 1000 663*41 297.70 SUPPORT126 10.50 666.23 298s06 SUPPORT127 10.50 669.05 298.4+2 SUPPORT128 10,50 671.86 29678 SUPPORT129 10.0 674.68 299.14 SUPPORT130 100bO 677.50 299.50 SUPPORT131 13.UO 638,50 294945 SUPPORT132 15.50 638950 294.40 SUPPORT133 18.00 638,50 294.20 SUPPORT134 20,50 638o50 294sU0 SUPPORT135 23.00 6'J&950 293.6U SUPPORT136 25.50 630.50 293.20 SUPPORT137 28.U0 638,50 292.25 SUPPORT13d 30.0 630,50 291930 SUPPORT139 1300 663.41 297070 SUPPORT

140 15.0 663.41 297s70 SUPPORT141 18.00 6b6*41 297.70 SUPPORT142 20.50 663.41 297965 SUPPORT143 230U0 663o41 297,60 SUPPORT

144 25.b0 663.41 297.50 SUPPORT

s -1 ECODE IDENT -DWG NO.

. . 4 n " _..649-2924-001

SCALE IREV SET 57

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145 28.00 663.41 297.40 SUPPORT146 30.50 663.41 297.30 SUPPORT

147 13,00 677.50 299.50 SUPPORT148 15.50 677.50 299.50 SUPPORT149 18.U0 677.50 299.50 SUPPORT150 20ob0 677.50 299.50 SUPPORT151 23.00 677.50 299.50 SUPPORT152 25sb0 677.50 299.50 SUPPORT

153 28,00 677.50 299*50 SUPPORT

154 309b0 677.50 299.50 SUPPORT

NODE RELEASES

101 TO 115 FORCE Y MOMENT Y116 TO 130 FORCE X Y MOMENT Y131 TO 138 FORCE X y MOMENT X139 TO 146 FORCE X147 TO 154 FORCE X Y MOMENT X

SIZE CODE IDENT DWG NO.

A 13 9 649-2924-001SCALE REV SHEET 58

4 1

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TYPE BENUING

ELEALNT 11CIDENCES

1 2 38 1 52 61 72 602 38 58 37 53 72 61 b3a b8 38 2 54 72 65 744 58 2 3 55 b3 76 745 4 58 3 56 b3 65 766 58 4 62 57 76 65 787 62 4 5 58 42 41 788 6 62 5 59 78 65 429 62 6 64 60 42 65 4310 64 6 7 61 67 42 4S11 8 64 7 62 42 67 8012 64 8 66 63 41 42 8013 b6 8 9 64 67 82 8014 b6 9 46 65 67 69 821b 66 46 45 66 82 69 8416 46 9 10 67 84 69 8617 11 46 10 68 69 50 b618 11 68 45 69 b0 69 3119 46 68 45 70 86 50 8820 12 68 11 71 68 50 4921 68 12 7U 72 bc 32 3322 70 12 13 73 b5 32 5623 14 70 13 74 32 55 6124 70 14 54 75 56 59 b525 54 14 15 76 b9 16 bi6 70 54 53 17 bO 71 b927 58 36 37 78 71 60 7228 57 36 b8 79 72 75 7129 36 57 S5 80 74 73 7230 58 61 57 81 74 75 7331 61 58 62 82 75 74 7632 64 61 62 83 78 75 7633 61 64 63 84 75 78 7764 64 65 63 85 77 78 4855 65 64 66 d6 40 7 '41£6 65 66 44 87 40 19 7767 65 44 43 88 40 79 ,)38 44 66 45 89 80 79 4039 b8 44 45 90 80 40 4140 68 67 4q 91 03 bl 7941 44 67 43 92 ul 80 di242 68 69 67 93 b4 (51 d243 69 6d 70 94 i bi b344 70 52 69 95 4b3 b645 b2 70 56 96 85 04 t646 69 b2 bl 97 b5 bo Do

57 b7 34 65 98 35 63 8748 b56 34 t749 64 56 6J50 61 b6 b7b5 !6 61 60 SIZE CODE IDENT DWG NO.

SCALE REV SHEET

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044

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SCALE IREV S HEET 60

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99 88 48 87OO 48 88 49

101 31 17 16102 31 55 17103 17 55 18104 55 19 18105 55 59 19106 19 59 20107 59 21 20108 59 71 21109 21 71 22110 22 71 75111 73 23 22112 23 73 75113 75 24 23114 24 75 77115 39 24 77116 24 39 25117 39 26 25118 26 39 79119 81 26 79120 26 81 27121 27 81 63122 27 83 28123 28 83 85124 85 29 28125 87 29 85126 29 87 47127 29 47 30128 47 87 48

SIZE CODE IDENT D)WG No.

19 649-2924-olSCALE IREV SHEET_61

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SUMMARY

A STRESS ANALYSIS WAS PERFORMED ON THE ANTENNA ADAPTER MOUNT (649-2848-001)

UNDER WHAT WAS CONSTDERED A WORST CASE AERODYNAMIC LOADING CONDITION OF THE

ANTENNA. THE ANALYSIS OF THE CASTING SHOWS THAT IT IS OF SUFFICIENT

STRENGTH TO CARRY ALL INDUCED LOADS WITH THE FOLLOWING MARGINS-OF-SAFETY

(CASTING FACTOR OF 2.0 INCLUDED):

MS (CASTING TENSILE YIELD) = +2.24

MS (CASTING SHEAR ULT) = +11.2

MS (ATTACHMENT BOLTS TENSION) = +30.4

SIZE CODE IDENT DWG NO.SIE13499

SCALE RE SHEET

1A7 IAA

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'AD-A095 634 ROCKWELL INTERNATIONAL DALLAS TEX COLLINS RADIO GROUP P/6 1/3STRESS ANALYSIS OF AIRCRAFT MODIFICATIONS (C-11R AIRCRAFT). JO--ETC(U)OCT 80 D B RAGAN FO9603-80-C-0602

UNCLASSIFIED NLe mmIm2ImuuullfllfllllEIIEEEIIEIIIIIEIIIIIEEEEIIEE

Page 99: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

TABLE OF CONTENTS

SECTION PAGE

1.0 INTRODUCTION 98

2.0 LOCATION OF THE NODE POINTS 100

3.0 LOCATION OF THE FINITE ELEMENTS 106

4.0 PROPERTIES OF THE STRUCTURAL COMPONENTS 115

5.0 LOADING OF THE CASTING STRUCTURE 116

6.0 MISCELLANEOUS ANALYSIS AND EXCUTION STATEMENTS 120

7.0 RESULTS OF THE COMPUTER ANALYSIS 121

8.00 FORCES INDUCED INTO THE AIRCRAFT 126

APPENDICES

A AERODYNAMIC LOADING CALCULATIONS

B LISTING OF COMPUTER RESULTS

ISZE CODE IDENT DWG NO.

A 134 991 649-2924-001

SCALE ]REV ISHEET 96

074-8679-140 4

Page 100: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

'C14I-Bs DM C34-3/B UHF AIJTENNA MOD#

* ICES STRUDL-11 *

** THE STRUCTURAL DESIGN LANGUAGE *

CIVIL ENGINEERIN( SYSTEMS LABORA'IOY *

* MASSACHUSLTTS INSTITUTE OF TECHNULOGY *

*CAMbRIDGEt MASSACHUSETTS. . . . . _ .- . - . * - - -

* 17*1'&.36 22 AUG 80 *

* UNIVAC 1100 SEnIES EXEC 8 *

-------- VLRSION 2,7 ,

PREPAi LU BYT MAARTEN VET

1W047-oA OF M72-r1A'A

SI ZE CODEIDENT DWG NO. 6922-0A L13 99 I 649-2924-001

S L EI R E V I S H E E TI9 7

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1.0 INTRODUCTION

A STRESS ANALYSIS WILL BE PERFORMED ON THE ADAPTER CASTING WHICH IS

THE TRANSITION BETWEEN THE DM C34-3/B UHF ANTENNA AND THE FUSELAGE

OF THE C141-B AIRCRAFT. THE ADAPTER WAS ADDED TO COMPENSATE-FOR THE

7-DEGREE FORWARD SLOPE OF THE FUSELAGE; THUS THE ANTENNA WILL FLY

WITH A ZERO ANGLE OF ATTACK. THE LOADINGS TO BE CONSIDERED ARE THE

AERODYNAMIC FORCES INDUCED DUE TO EITHER THE MAXIMUM PERMISSIBLE

VELOCITY OF 380 KNOTS AT SEA LEVEL OR MACH 0.85 ABOVE 23,000 FEET

ALTITUDE; WHICHEVER PRESENTS THE WORST CASE CONDITION. HOWEVER, TO

ENSURE THAT A CONSERVATIVE ANALYSIS IS PRESENTED, THE AERODYNAMIC

FORCES WILL BE CALCULATED FOR AN ARBITRARY 10-DEGREE ANGLE OF ATTACK;

SUCH AS MANY BE ENCOUNTERED DURING TAKEOFF OR SHARP MANUEVERING IN

FLIGHT.

THE CASTING WILL BE MODELED USING TRIANGULAR PLATE ELEMENTS FOR THE

BASIC CASTING WALLS AND TRIDIMENSIONAL ELEMENTS FOR THE HOLD-DOWN

BOSSES. THE CASTING MATERIAL IS ALUMINUM ALLOY A356-T6.

SIZE CODE IDENT DWG NO.

A 134 99 649-2924-001

SCALE REV SHEET 98

n74-RA7Q1dn

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E9

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M OCSIZE COE IDINItWG -NO

A 13499 69-294-00

SCALE~~N IRVSET 9

Page 103: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

2.0-LOCATION OF THE NODE POINIS

UNITS INCHES,0DEGRELS.

2.1--LOwER SLOPING PLANE

NODE COOMOINATES

x-. y z

1 -1.06 +0.00 -0132 --- 0.75 -1.31 -009-a 00.00 -2.25 0.004 0O.04 -2.88 0.125 02.06 -3.50 0.25 ------ .4 05obB -2.63 0.696 02.76 -3.50 0.34 45 06.458 -2.63 0081.7 03.76 -,3.50 0.'#6 '46 12.00 -2.65 1.478 0 5obS -3.50 0.69 47 - --- 15.UU -2.63 1.609 06ob8 -5.50 0.81 4d8 14.63 -2.63 lobO10 09.68 -3.50 1.15 49 15.63 -2.b6 1.9211 12.00 -3.50 1.47 -. . . . .50 - -- 18.88 -2.25 2.46212 13*UO -3.50 1.6U 51 19.75 -1.69 2.'4213 14.63 -3.50 1.80 52 009bO +1.50 0.0614 15.63 -3.50 1.92 b3- - --- o oi68 +2.13 0 c1715 18ob6 -3.50 2.208 5'# 02.16 +2966 0.6'%16 19.51 -5.00 2.37 55 03.76 +2.65 0.46

.17 -20.*25 -2.38 2.49 - .56 -05.bb +2.63 0.6918 21.25 -1.31 2.61 57 06*53 +29b3 0.8119 21.56 +0,00 2.65 50 12.00 +2.63 1.4720 .09.638 -2.63 1.15 ----- 59....3oUO +2.63 1.6021 09.38 +0.00 1.15 60 14.63 +2.63 1.8022 -0.15 +1.61 -.09 61 15ob6 +2.63 1.9223 -00,00 +2.25 0.00 .--- 62 18.8B +.925 2.6224 00e94 +2.88 0.12 63 19.75 +1.69 2.4225 02oU6 +3.50 0.25-26 02.76 +3950 0.34 ..-

27 03.76 +3.50 0.4628 05.b8 +3,50 0.69

-29 ... 06.58 +3.50 0.81 -

3b 08 +3.50 1.1531 12.00 .6*bD 1.4732 13.UO 4-3.50 1.60 .-

33 14005 +3.50 1.8064 15.63 +3.50 1.92-3 5 -16.56i +3.50 2.28 - -

36 19.61 +3.00 2.3737 20.25 +2.38 2.4938 -2192b +1931 2.61 . -.

39 09s68 .2.63 1.15'*0 00.0 -1.50 006411 01.58 -2.13 0.17142 02.76 -2.63 0.34'#5 03.76 -2.63 0.46 SIE CDE IDENT DGNO.

A 11 4991649-2924-001

SCALE jREV ISHEET 100 __

---. -----

Page 104: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

__.-( oo.oo

-

.NV?-0

AiA

V1i

cl' I 4 %A ®r

p4 /C0 N0

~bbNo

00-00

901-

( C4C , N o S Z E C Q E D E T I U G O 6 9 - 9 4 - 0I 139

ISCL REIS ) 0

Page 105: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

2*i--UPPiLR PLANE

NODE COUOiINATES

101 -1.U6 .0.00 3.20102 .-0.75 -1.31 6.20103 00*UG -2*2b 6.20104 00*.04 -2.88 3.20105 (12.06 -3.50 5.20 .150 .88ob .2.25 5.2010b 02.'16 -3.50 3.20 151 19*15 -1.69 3.2030? 03.76 -3.50 3.20 - 152 00.50 .1.50 6.20108 0 5* 8 -3.50 3.20 -- *-* - - 155 - --01.68 .2.13 6.o20109 U06.:8 -5.50 5.20 154 02s76 +2.63 3.20110 09.08 -3.0 3.20 155 03,16 +2o63 3.20III 12.00 -3.50 3.20 - - .156 - 05*t'8 +2.63 3.20112 15.00 -3.50 3.20 - * 151 06.58 +2.63 3.20115 14.63 -5.50 3.20 155 12.00 +2#63 5.20

-114 - 15.63 -3.50 3.20 - - 159 - -15.00 +2.63 3.20115 18.56 -3.50 3.20 160 14.63 +2963 3.20116 19.61 -3.00 5.20 161 15.65 +2.65 3.20117 20 *0.25 -2.3b 3.20 - **- 162 18.88 +2.25 3.20118 21.25 -1.31 3.20 163 19.75 +1*69 6.20119 210*6 +0.00 3.20 165 02.06 .0,00 3.20

*120 -- 09*18 -2.63 3.20 - 164 00,UO +0.00 .3.20121 09.68 +0.00 3.20 166 04.74 .0.00 3,20122 -0.15 +1.31 6.20 167 07.'41 +U,00 3.20 .

123 00.00 +2.25 6920 - -- 168B 11.41 +0.00 3.20124 (0.94 +2.88 3.20 169 13.89 +0.00 3020125 02.,)6 +3.50 5.20 170 15.63 +0s00 15.20

-126 -02.76 +5.50 5o20 -171 18.56 +0.00 3.20127 03.76 +3.50 3.20 172 00.00 -1.31 3.20128 05.58 +3.50 3.20 173 029UJ6 -2.63 3.20129 -06.58B .3.50 6.20 -.--- 174 04.74 -2.63 5.2b130 09.08 +6.50 6.20 175 07.41 -2.63 3.20131 12.00 .3.50 3.20 176 11.41 -2.63 3.20*132 -13.00O .3.50 3.20 17? 13.89 -2.63 5.20133 14.65 +3.50 3.20 1713 18.56 -29b3 3.20134 15.63 .5.50 3.20 179 00.00 +1.31 3.20135 16.56 +3.50 3.20 180 02.06 +2.65 3.20*136 19.01 .3*00 3.20 181 04.14 +2.63 3.20137 20.25 .2*38 3.20 182 07.41 +2.65 6.2013d 21.25 .1.31 3.20 186 11.41 +2.635o320139 09.08 +2o65 3.20 18'4 13.69 +2.63 3.20140 00.50 -1.505.*20 - - -18 18.56 +2.63 5.20141 01.68 -2.13 6.20 -- ~ *--186 -16.57 -2.63 3.20142 02076 -2.63 3.20 187 16.67 +2963 3.20146 03@76 -2.63 3.20144 05.b8 -2.63 3.20145 06.58 -2.63 3.20146 12.00 -2.63 3.20147 13.00 -2.63 3.20148 14963 -2963 3.20 F ~~IETjW O

* 1~ 5.b -. 635.0 A 1134991I 649-2924-001

SCALE 'IREV ISHEET 102

Page 106: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

kA4)

9I oz

00 /

SZCODE IDENT jDWG NO.

A 1149 649-2924-001

SCALE lREV _JSHEET 10

Page 107: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

t44

I'4,

40

C1510

SIZE -CODE IDENT DWG NO.

A 113499 649-2924 -001

SCALE IREV SHEET 104

Page 108: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

293--SUPPO(I.NUODES

NODE COUNDINATES

x y z

220 09.68 -2.63 0,15 SUPPORT221 09.36 +0.00 U,15 SUPPORT259 09948 +2.6b 0.15 SUPPURT240 0o.o~ -1.50 -.94 SUPPORT241 01,68 +2013 085 SUPPORT242 02,76 -2960 "*g6 SUPPORT

243 0.76 -2.63 -. 54 SUPPORT244 0S -2.63 -. 51 SUPPORT245 06!8 -2.63 -19 SUPPORT246 2.1)0 -2.63 0.47 SUPPORT247 1300 -2.63 0.60 SUPPORT248 .14b3 -2.63 0.80 SUPPORT249 15.63 -2.63 0.92 SUPPORT250 18.b8 -2.25 1,32 SUPPORT251- 975 -1.69 1.42 SUPPORT252 00.b8 +150 -994 SUPPORT256 10..58 +213 -83 SUPPORT254 02.6 +2o63 -966 SUPPORT

255 03.76 +2.63 -e54 SUPPORT256 057B +2.63 -.31 SUPPORT255 U6,8 +2#63 -15 SUPPORT258 12.00 +2.63 0.47 SUPPORT259 13.U +2.63 0.60 SUPPORT26U 149b3 +2.b3 0.80 SUPPORT261 15.63 +2.63 0.92 SUPPORT262 18,b8 +2.25 1.32 SUPPORT263 19.75 +1969 1942 SUPPORT

NOOE - RELEASES

22U9239 FORLE Y240 iD 263 -FORCE Y

SIZE CODED.NT DWG NO.j~~ 9 I649-2924-001SCALE IREj ISHEET 105

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30--LOCATION OF THE FINITE ELEMENTS

3*1--UiPPER HORIZONTAL SURFACE

TYPE BENUING

ELEMENT INCIDENCES

1 101 172 1642 172 101 102

102 103 172

4 172 103 1405 104 173 1416 175 104 1057 106 173 1058 173 106 1429 107 174 14310 107 108 17411 174 108 14412 109 175 14513 109 110 17514 175 110 12015 110 176 12016 110 111 17617 176 111 14618 112 177 14719 112 113 177 .20 177 113 14621 114 186 14922 114 115 186165 156 115 17823 115 116 17824 17d 116 15025 118 151 11726 119 151 11827 163 119 13828 130 137 16329 136 18b 16230 185 136 13531 135 134 18732 187 134 161166 135 187 185- -. -

33 133 184 16U34 133 132 18435 184 132 15936 131 183 15837 131 130 18338 183 130 13939 130 182 13940 130 129 15741 182 129 157 SIZE CODE IDENT DWG NO.42 128 181 156 0 3/,Q9 649-2924-001

SCALE IREV [SHEET 106o/, A

Page 110: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Ms I/ z

I 'lk

11-4

901-40 t

-- SIZE CODE IDENT DWG NO.A 113 4.S'9 649-2924-001

SCALE IREV jSHEET 107

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43 128, 127 181 78 170 150 17144 181 127 '155. 79 171 150 15145 126 180 154 80 119 171 15146 18( 126 125 81 171 119 16647 125 124 110 82 162 171 16348 180 124 153 83 162 170 17149 123 179 152 84 170 162 18550 123 122 179 85 170 185 18751 101 179 122 __. 168._.171L- 87 16152 179 101 164 86 160 170 16153 172 165 164 87 170 160 169

54 165 172 140 88 169 160 18455 141 165 140 89 159 169 18456 173 165 141 90 159 168 16957 142 165 173 91 168 159 15858 143 165 142 92 168 158 18359 165 143 166 93 139 168 18360 166 143 174 94 168 139 16161 .144 166 174 95 139 167 12162 144 167 166 96 167 139 18263 167 144 145 97 157 167 18264 167 145 175 98 156 167 15765 120 167 175 99 167 156 16666 167 120 121 100 . 166 156 18167 120 168 121 ..... 101 155 166 15668 168 120 176 102 155 165 16669 146 168 176 106 165 155 15470 147 168 146 104 165 154 18071 168 147 169 10b 165 180 15672 169 147 177 106 152 165 15673 148 169 177 107 165 152 17974 169 148 170 108 165 179 16475 170 148 149167 186 170 14976 178 170 18677 170 *178 150

SIZE CODE IDENT DWG NOIA 113Air91 64922400

SCALE IREV ITSHEET 108

Page 112: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

I3,2--VERTICAL SIDE ELEMENTS

TYPE BENUING

ELEMENT INCIDENCES

109 1 102 101 155 1 122 101110 102 1 2 134 122 1 22111 5 102 2 135 25 122 22112 102 3 103 136 122 23 125115 4 105 104 137 24 125 124114 105 4 5 13b 125 24 25115 6 lob 5 139 26 125 25116 105 6 106 140 125 26 126117 7 108 107 141 27 121 127118 108 7 8 14a 128 27 26119 9 110 1U9 143 29 130 12912U 110 9 10 144 130 29 3u121 11 110 10 145 31 130 30122 110 11 111 146 130 31 131123 12 113 112 147 32 133 132124 113 12 13 148 133 32 33125 14 115 114 149 34 135 134126 115 14 15 150 135 34 35127 16 115 15 151 56 135 3512d 115 16 116 152 135 36 13b129 17 118 117 153 37 138 137130 118 17 18 154 138 37 38131 19 11 1d 155 19 138 38132 118 19 119 156 136 19 119

SIZE CODE IDENT DWG NO.

A 113499 649-2924-001

SCALE IREV ISHEET 109

Page 113: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

ri S

IV

IrI

ti

00 oar

SCLE .ISHEET 110

"S.

0?I ~ .

Page 114: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

3.3--CAST BOSSES

TYPE TRIUIMENSIONAL

ELEMENT INCIDENCES

200 3 4 104 103 40 41 141 140201 6 7 107 106 42 43 143 142202 a 9 109 108 44 4b 145 144203 11 12 112 111 46 47 147 146204 13 14 114 113 48 49 149 148205 16 17 117 116 50 51 IbI 150206 52 53 153 152 23 24 124 123207 54 55 155 154 26 27 127 12620d 56 57 157 156 28 29 129 128209 58 59 159 158 31 52 132 131210 60 61 161 160 33 34 134 133211 62 63 163 162 3b 37 137 136

SIZE CODEIDENT DWG NO.

A 1349 91 64929.ooSCALE IREV SHEET ill

I I_ _ _ __II

Page 115: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

394--TRANSVERSE NIB

TYPE BENLING

LLEMENT INCIDENCES

157 110 20 10158 20 110 120159 121 20 12016U 2U 121 21161 121 39 21162 39 121 139165 130 39 13916' 39 130 30

!ii

/0 120 2

• (n I f

SIZE COIDE IDENT jDWG NO.134 99 649-2924-001

SCALE J}REV ISHEET 112I I ii I

Page 116: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

35--SUPPOAT MEMdERS

TYPE SPACE FRAME

MEMdER INCIDENCES

300 220 20301 221 21302 239 39305 240 40304 241 4L305 242 42306 245 435 .....

307 2414 44308 245 4b-309 246 46

310 27 47311 28 4312 249 59316 250 50314 251 51315 252 52.. . . . . . . . . . . . . -

316 253 55317 254 54318 25b 55

319 256 56320 257 57321 258 58322 259 59323 260 60324 261 61325 262 62326 263 65

SIZE CODE 100N0 DWG NO.

A 134, 9 649-2924-001

SCALE IREV - ISHEET 113

A ____ _____

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i . .. ,

3.b--DUMMY FRAMING MEMBERS ...

IN ORUER TO HAVL COMPATIBILITY-OF DEGHELS-OF-FREEDOM AT ALL THE

NODE PUINTS9THIN DUMMY MEMBEhS WILL BE USEU TO MAKE UP A VIRTUAL FRAME

HAVING INSIGNIFICANT STIFFNESS. -...

TYPE SPACE FRAME

MEMBER INCIDENCES

40U 1 2401 2 3 437 101 102402 - 3 4 . . . . . . ; - 102 105 .. . ..... ... . .

406 4 5 439 105 104

4u4 b & 440 104 105 475 1 101

405. 6 7 .4.41 -o10b 10 .. .474 - 2 102

406 7 a 44d 106 107 475 5 105

407 a 9 446 107 1U8 476 10 110408 4 9 10 ... . -. 108 109 .477- 15 115

409 10 11 445 109 110 478 18 118

410 11 12 44b 110 111 79 19 119

411 12 1 447 111 112 48U 22 122

412 16 14 44B 112 115 481 2b 125

416 14 15 449 115 114 482 30 150

414 NOT USED "450 -- 114 115 4 s 35 13!a

41b lb 16 451 115 116 484 38 168

416 16 17 452 116 11741- 17 S 456 . 117 118.41b 1S 49 4b4 118 119

419 1 22 45o 101 122420 22 25 bb 122 226

421 23 24 457 123 124

422 24 25 455 124 125

426 25 26 . 5 -" 125 12b

424 26 27 46U 126 127

42b 27 28 461 127 128

-426 28 29 .462 -- 128 129-

427 29 30 463 129 130

42b 30 31 464 130 131

429 31 32 .465 131 1S.

430 32 33 466 132 136

431 36 34 467 136 154

432 34 35 4.... .. -468 .134 155 -.. ...

436 35 36 469 135 136

434 36 37 470 156 137

435 3? 38 471 137 18

46b 30 29 119

SIZE CODEI DENT DWG NO.

A 1345.)5.9 649-2924-001

SCALE IREV ISHEET 114

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490--PROPERIIES OF THE STRUCTURAL COMPONENTS

ELEMENT PROPERTIES

1 TO 108 TYPE ISBCTI THICKNESS .190109 TO 114 TYPE 'SBCTv THICKNESS 6375115 TO 120 - TYPE ISBCTI THICKNESS .190-129 TO 132 TYPE IsuCit THICKNESS 1-25166 TU 158 TYPE ISBCT9 THICKNESS *67b139 TO 152 TYPE OSCTO THICKNESb .190lb6 TU 156 TYPE ISBCTf THICKNESS 1.25157 TO 164 TYPE *SBCT' THICANESS 1.0U16b TO 168 'TYPE ISBCT' THICKNESS .190

200 TO 211 TYPE lIPLSCSH-

MEMBER .. PROPEKTIES- _ _

300 TO 326 'AX s0228 IX *0002 1Y #0001 SY .0007 IZ .0001 SZ .0007

400 TO 413 AX s0361 IX *0002 IY .0001 Iz .0001415 TO 484 AX 90661 IX .0002 IY fOU01 Iz .0001

CONSTANTS

E I*UUE7 ALLG 39OOE6 ALLPOISSUN .63 ALL

E 2*V0E7 300 TO 326G- 1920E7 300 TO 326POISSUN .60 300 TO 326

SIZE CODE IDENT -j W NO. 6 9 2 2 -0A 134991 ,4,.924.0o,SCALE REV , SHEET 115

Page 119: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

5.0--LOADING OF THE CASTING STRUCTURE

THE LUADING To BE APPLIED IS FOR THE SEA LEVEL FLIGHT AT THE

MAXIMUM VELOCITY OF 38U-KNOTS. THIS CONDITION RESULTS IN THE WORST-

CASE DYNAMIC LOADING.

DKAG FORCE 90.90-LB.

LIFT FORCE 3389.0-LB.

MUMENI 2360 IN,-LB.

LOADING 'DRAG'

NODE LOADS

172o179 FORCE X +5.68 FORCE Z +42.82

173.180 FORCE X +5.68 FORCE Z +40.41

174i.181 FORCE X +5.68 FORCE Z +37.28

17b.182 FORCE X +5.68 FORCE Z +34.16

176.186 FORCE X +5.68 FORCE Z +29.49

177.o14 FORCE X +5.68 FORCE Z +26959

186.187 FORCE X +5,68 FORCE Z +23o69

17Ue185 FORCE X +5.68 FORCE Z -65144

SIZE CODE ID ENT DWG NO.A 134& 649-2924-001[13 4.A )I9

SCALE IREV _ SHEET 116

...... , ,,, r . .,. ......... .... ........ . ..... .. .... . . . ..A.

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A1 S'SCI1 ' 770 (V: 77le ,o4'7-WV1-7 ~ s/ O 4//

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S A 1~~r~vax Ai SIZE CODE IDENT DWG NO.c~ S A 13 ~9 649-2924-001

SCALE - REV ISHEET 117

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.2 F ,O - 1i3 , 8 2) -fi

+ (4., ') (2.,0 9)

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IVNOOE5 / 3J)4 FelZcc X-:- -5,66

r66 C---Z -~2/.3*i4. ('0 1)+ -4 4-I

ATOO.-S 1741/p F -'zc' =x 4S.C'F# e -(2/./3 f //_1 2e,) Zl

For.cc- "2= vz,/3 -- '' (21, K 9) 7- 4 3,1 V,

ej 6 T

FORC4 2 2 " /,13 1('" VL(21, eJ- 2 .

SIZ E CODE IDENT DWG NO.

S.3499 649-2924-001

SCALE IREV ISHEE T 11

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MvOOE"S 177 /8+! f" ew tC-- I5.

S;2:23,6?

Aroo /7 3 1 o R ref ' X f""5g

Fo , r4 2 '.- 2 31,4-

-41

SIZE CODE IDENT DWG NO.

A 1134991 649-2924-001

SCALE IREV "(SHEET 119 I______________

Page 123: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

6.O--t4ISC. ANA~LYSIS AND-EXECUTION STATEMENITS

STIFFNESS AI'ALYSIS R~EDUCE BANU ROOT

UNITS KIPS

OUTPUT DECIMAL 3

LIST FORCEStREACTIONSSTRESSES ALL

FINISH

SIZE CODE IDENT DWG NO.

A 134 11 649-2924-001

SCALE IREV ISHEET 120I

Page 124: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

Z.0 -AeiQ7 r74 ~~P'Z?/-,?

7 / R - --5 S a4 s/( sV ? 6V7/v

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Ai~A ~*O,,cr ~~s #~7f 3 5 ,'r ~ 24-

M~I -8C ec~ AlJqd 5&-77- 04 I'c-lv-1 A-, +

4 V- 7 lZ-5U e ACM6

/W/ K - (77)(4rs ) 5" : -7 / -Z

/V/Ay. O1Rd-c7 5-7?2-!S5 132.6-P51 /'V h:Z. 12,a

SIZE CODE IDENT D WG NO.

,0 a649- 2924-001

SCALE REV SHEET 12_ _ _

- ______121

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A ? c-43"1 1. iIrnc "0,T oF 2. 0 Lv-z // 6w / U3 6-0

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SSIZE CODE IDENT DWG NO.

A 13499 649-2924-001SCALE REV SHEET 122

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SIZEOD DET DWG NO.lei a 9 9 1,,.9,.0A113 %06649-2924-001

SCALE IEV ISHEET 123

b*L -. .w-

Page 127: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

72- ,,77/C//A1,vT" 6,2T z s

RESULTANT JOINT LOADS - SUPPORTS

JOINT ---------------------- FORCES ---------------------X FORCE Y FORCE Z FORCE

220 GLO -0010 o000 0-007221 GLO -.009 -,0Uo -007239 GLO -.011 .000 -s007240 GLO -OOX .000 -. 038241 GLO -. 002 .000 -. 034242 GLO -003 uo0 ,02243 GLO -o003 .000 -.016244 GLO -0003 .000 -0282145 ...... GLO .. -003 .000 -.012246 GLO -.001 .000 -022247 GLO -. 001 .000 -. 010248 ...... GLO -0002 UO0 -. 015249 GLO -. 002 .000 -.007250 GLO - 9004 .000 ,050261 . .. . . GLO ... -.... .005 .000 ,.002252 GLO -.001 .00"0 -. 037253 GLO -*002 .000 -. 033254 -. GLO ... -003 .000 -,028255 GLO -000 .000 -001525b GLO -005 ,000 -*028

- 257 -LO -003 .U0 0015258 GLO -.002 .000 -. 021259 GLO -,002 000 -. 010

----- 260---------. GLO -.002 .000 -. 016261 GLO -,002 000 -. O06262 GLO .004 ,000 0'%263 . GLO -005 000 -.003

TOTALS -0091 -. 0UO -4338

7-c' 7/6-- 9111Z- Y7/1,71-2 0v 4 1- r A e4'- ... ...

(-/, 3vso~ 3 34 72 4?

SIZE CO IDENT |DWG NO. - - 001

|A I 1I . 9 94SCALE IREV . . SHEET 124

Page 128: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

AIV 3 ROZ-77s 06o-32)p..s1= 22 -t

YIMC6- 77/C 3"tI 9 /5 /f Af5/CiV/pF/ez#'v l/4rWT/2C77dM

Z-9 0/l 776 ,VS 'zz ,'7- 6.- vreo.

M.s'. ( " ' cu 7 ) -- 4 So,. 72--

SIZE CODE DET DG NO.

A 1349 9 649-2924-001

SCALE jREV ISHEET 125A

Page 129: ROCKWELL INTERNATIONAL DALLAS TEX COLLINS FIG STRESS

e- FhcES /AOUIC-1T //VW7Z 77/t- /7/,RC?P-7-

8.1 ,1SL),UP770ff S

* Duci 7-D 72/,c r~7;7rA,,A-sS e-F 771z-/C ,-vn---v-81-7X' IV477 ) Irv caO 41) r?/J/ 727 77/1~ &41v41t1*w

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C,2S-76 FK-t-7 Z VC d1 47/ WI / CPR4" 7T- 77/C

SCALE REV SHEE 12C10A

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APPENDIX A

AERODYNAMIC LOADING CALCULATION4S

~SIZE CDE IDENT JDWG NO.A 1 349c,,,9 I649-2924-001 1

SCALE (REV SHEET A- I_ __

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APPENDIX B

LISTING OF COMPUTER RESULTS

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SCALE ]REVSHT I

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