Engineering Mechanics Dynamics SI Edition 4th Edition by Pytel and Kiusalaas Solution Manual

Page 1

Chapter 12 12.1 y = −0.16t4 + 4.9t3 + 0.14t2 m v = ẏ = −0.64t3 + 14.7t2 + 0.28t m/s a = v̇ = −1.92t2 + 29.4t + 0.28 m/s2 At maximum velocity (a = 0): −1.92t2 + 29.4t + 0.28 = 0

t = 15.322 s

vmax = −0.64(15.3223 ) + 14.7(15.3222 ) + 0.28(15.322) = 1153 m/s y = −0.16(15.3224 ) + 4.9(15.3223 ) + 0.14(15.3222 ) = 8840 m 12.2 1 (a) x = − gt2 + v0 t ∴ v = ẋ = −gt + v0 ∴ a = ẍ = −g 2 When t = 0, then x = 0 and v = v0 . Hence v0 is the initial velocity. Since gravity is the only source of acceleration in this problem, g must be the gravitation acceleration. v0 (b) When x = xmax then v = 0. ∴ −gt + v0 = 0 ∴ t = g 2 v0 1 v0 v2 ∴ xmax = − g + v0 = 0 2 g g 2g 1 2v0 ∴ − gt2 + v0 t = 0 ∴ t = 2 g (26.8)2 2(26.8) = = 36.6 m ∴ t = = 5.46 s 2(9.81) 9.81

At the end of flight x = 0. (c) ∴ xmax 12.3

x = 6 1 − e−t/2 m 1 −t/2 v = ẋ = 6 e = 3e−t/2 m/s 2 1 −t/2 = −1.5e−t/2 m/s2 a = v̇ = −3 e 2 5 c 2017 Cengage Learning. All Rights Reserved. May not be scanned, copied or duplicated, or posted to a publicly accessible website, in whole or in part.


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