12
Massa anak timbangan= 87.01 gram Massa beban tambahan: m1 2.9 gram m2 7.9 gram m3 10.8 gram no m Sbc Sab 1 2.9 0.3 0.3 0.35 0.4 2 7.9 0.3 0.35 0.4 3 10.8 0.3 0.35 0.4 beban tambahan pertama (m1) NO Sab t rata-rata a (m/s2) 1 0.3 1.82 0.09056877189 2 0.35 2.19 0.07297595963 3 0.4 2.4233333333333 0.0681135756 Σ 0.23165830712 beban tambahan kedua (m2) NO Sab t rata-rata a (m/s2) 1 0.3 1.1166666666667 0.24058810425 2 0.35 1.3033333333333 0.2060426083 3 0.4 1.63 0.15055139448 Σ 0.59718210704

Pengolahan Data Pesawat Atwood

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Page 1: Pengolahan Data Pesawat Atwood

PESAWAT ATWOODMassa anak timbangan= 87.01 gram jari-jari katrol=Massa beban tambahan: massa katrol=m1 = 2.9 gramm2 = 7.9 gramm3 = 10.8 gram

no m Sbc Sabt ab (detik )

t1

1 2.9

0.3

0.3 1.850.35 2.180.4 2.46

2 7.90.3 1.08

0.35 1.210.4 1.63

3 10.80.3 1.05

0.35 0.990.4 1.11

beban tambahan pertama (m1)NO Sab t rata-rata a (m/s2)1 0.3 1.82 0.090568771892 0.35 2.19 0.072975959633 0.4 2.4233333333333 0.0681135756

Σ 0.23165830712

beban tambahan kedua (m2)NO Sab t rata-rata a (m/s2)1 0.3 1.1166666666667 0.240588104252 0.35 1.3033333333333 0.20604260833 0.4 1.63 0.15055139448

Σ 0.59718210704

Page 2: Pengolahan Data Pesawat Atwood

beban tambahan ketiga (m3)NO Sab t rata-rata a (m/s2)1 0.3 1.0666666666667 0.2636718752 0.35 1.0733333333333 0.303807723473 0.4 1.1766666666667 0.28890369074

Σ 0.85638328921

NO g (m/s2) I g-g rata-rata I1 4.934837 5.4762998155752 13.05307 2.64193723498653 13.2455 2.8343625805884

Σ 31.23341 10.95259963115

percepatan gravitasi rata-rata ( g rata-rata ) = 10.4111365536 m/s2simpangan data hasil pengukuran = 3.65086654372 m/s2

kesalahan absolut = 3.65086654372 m/s2kesalahan relatif = 35.0669355352 %

nilai terbaik = 14.0620030973 m/s2

Page 3: Pengolahan Data Pesawat Atwood

PESAWAT ATWOOD0.0302 meter

29.6 gram

t ab (detik ) t bc ( detik )t2 t3 t rata-rata t1 t2 t3 t rata-rata

1.79 1.82 1.82 1.07 1.73 1.17 1.32333333332.22 2.17 2.19 1.2 1.16 1.2 1.18666666672.37 2.44 2.4233333333 1.01 1.14 0.98 1.04333333331.09 1.18 1.1166666667 0.54 0.54 0.63 0.571.49 1.21 1.3033333333 0.45 0.61 0.7 0.58666666671.61 1.65 1.63 0.51 0.45 0.45 0.471.08 1.07 1.0666666667 0.62 0.48 0.57 0.55666666671.05 1.18 1.0733333333 0.48 0.41 0.48 0.45666666671.11 1.31 1.1766666667 0.51 0.45 0.38 0.4466666667

a rata-rata= 0.07721944 m/s2g = 4.93483674 m/s2

a rata-rata= 0.1990607 m/s2g = 13.0530738 m/s2

1.7 1.8 1.9 2 2.1 2.2 2.3 2.4 2.50

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.162958665119443 x + 0.000544195910527512R² = 0.983183946220639

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

1 1.1 1.2 1.3 1.4 1.5 1.6 1.70

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.190092165898618 x + 0.0933755760368661R² = 0.975806451612903

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

Page 4: Pengolahan Data Pesawat Atwood

a rata-rata= 0.2854611 m/s2g = 13.2454991 m/s2

1 1.1 1.2 1.3 1.4 1.5 1.6 1.70

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.190092165898618 x + 0.0933755760368661R² = 0.975806451612903

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

1.06 1.08 1.1 1.12 1.14 1.16 1.18 1.20

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.722979552093475 x − 0.449294060370009R² = 0.795277507302824

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

Page 5: Pengolahan Data Pesawat Atwood

1.7 1.8 1.9 2 2.1 2.2 2.3 2.4 2.50

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.162958665119443 x + 0.000544195910527512R² = 0.983183946220639

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

1 1.1 1.2 1.3 1.4 1.5 1.6 1.70

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.190092165898618 x + 0.0933755760368661R² = 0.975806451612903

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

Page 6: Pengolahan Data Pesawat Atwood

1 1.1 1.2 1.3 1.4 1.5 1.6 1.70

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.190092165898618 x + 0.0933755760368661R² = 0.975806451612903

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

1.06 1.08 1.1 1.12 1.14 1.16 1.18 1.20

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.722979552093475 x − 0.449294060370009R² = 0.795277507302824

Chart Title

Column CLinear (Column C)

t (sekon)

s (m

eter

)

Page 7: Pengolahan Data Pesawat Atwood

PESAWAT ATWOODMassa anak timbangan= 87.01 gram jari-jari katrol=Massa beban tambahan: massa katrol=m1 = 2.9 gramm2 = 7.9 gramm3 = 10.8 gram

no m Sab Sbct ab (detik )

t1

1 2.9

0.3

0.3 1.850.35 2.180.4 2.46

2 7.90.3 1.08

0.35 1.210.4 1.63

3 10.80.3 1.05

0.35 0.990.4 1.11

m1 a = 0.077219435708

no Sbc Vbc1 0.3 0.27852279532 0.35 0.39417541453 0.4 0.571872623

m2a = 0.199060702347

no Sbc Vbc1 0.3 0.9980353982 0.35 1.11652836743 0.4 1.743549227

0.25 0.3 0.35 0.4 0.45 0.5 0.55 0.60

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.335881499648702 x + 0.210657227423089R² = 0.985307800365763

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

0.9 1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.80

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.116125263871181 x + 0.200658536902987R² = 0.865729901108046

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

Page 8: Pengolahan Data Pesawat Atwood

m3a = 0.285461096404

no Sbc Vbc1 0.3 1.01585196152 0.35 1.16979900893 0.4 1.871257924

0.9 1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.80

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.116125263871181 x + 0.200658536902987R² = 0.865729901108046

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

0.8 1 1.2 1.4 1.6 1.8 20

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.102857420309037 x + 0.210905605564635R² = 0.87984850620233

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

Page 9: Pengolahan Data Pesawat Atwood

PESAWAT ATWOOD0.0302 meter

29.6 gram

t ab (detik ) t bc ( detik )t2 t3 t rata-rata t1 t2 t3 t rata-rata

1.79 1.82 1.82 1.07 1.73 1.17 1.323333332.22 2.17 2.19 1.2 1.16 1.2 1.186666672.37 2.44 2.4233333 1.01 1.14 0.98 1.043333331.09 1.18 1.1166667 0.54 0.54 0.63 0.571.49 1.21 1.3033333 0.45 0.61 0.7 0.586666671.61 1.65 1.63 0.51 0.45 0.45 0.471.08 1.07 1.0666667 0.62 0.48 0.57 0.556666671.05 1.18 1.0733333 0.48 0.41 0.48 0.456666671.11 1.31 1.1766667 0.51 0.45 0.38 0.44666667

0.25 0.3 0.35 0.4 0.45 0.5 0.55 0.60

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.335881499648702 x + 0.210657227423089R² = 0.985307800365763

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

0.9 1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.80

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.116125263871181 x + 0.200658536902987R² = 0.865729901108046

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

Page 10: Pengolahan Data Pesawat Atwood

0.9 1 1.1 1.2 1.3 1.4 1.5 1.6 1.7 1.80

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.116125263871181 x + 0.200658536902987R² = 0.865729901108046

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title

0.8 1 1.2 1.4 1.6 1.8 20

0.050.1

0.150.2

0.250.3

0.350.4

0.45

f(x) = 0.102857420309037 x + 0.210905605564635R² = 0.87984850620233

Chart Title

Column CLinear (Column C)

Axis Title

Axis

Title