Vector Mechanics for Engineers: Statics and Dynamics
Vector Mechanics for Engineers: Statics and Dynamics
12th Edition
ISBN: 9781259977251
Author: BEER
Publisher: MCG
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Chapter 9.6, Problem 9.183P

(a)

To determine

Find the principal mass moment of inertia of the cylinder at the origin O.

(a)

Expert Solution
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Answer to Problem 9.183P

The principal moment of inertia are K1=2.26γtga4_, K2=17.27γtga4_, and K3=19.08γtga4_.

Explanation of Solution

Given information:

Refer Problem 9.168.

Show the moment of inertia as follows:

Ix=18.91335γt8a4Iy=7.68953γt8a4Iz=12.00922γt8a4

Ixy=1.33333γt8a4Iyz=7.14159γt8a4Izx=0.66667γt8a4

Calculation:

Show the Equation 9.56 as follows:

{K3(Ix+Iy+Iz)K2+(IxIy+IyIz+IzIxIxy2Iyz2Izx2)K(IxIyIzIxIyz2IyIzx2IzIxy22IxyIyzIzx)}=0

Substitute 18.91335γt8a4 for Ix, 7.68953γt8a4 for Iy, 12.00922γt8a4 for Iz, 1.33333γt8a4 for Ixy, 7.14159γt8a4 for Iyz, and 0.66667γt8a4 for Izx.

[K3(18.91335γt8a4+7.68953γt8a4+12.00922γt8a4)K2+(18.91335γt8a4×7.68953γt8a4+7.68953γt8a4×12.00922γt8a4+12.00922γt8a4×18.91335γt8a4(1.33333γt8a4)2(7.14159γt8a4)2(0.66667γt8a4)2)K(18.91335γt8a4×7.68953γt8a4×12.00922γt8a418.91335γt8a4×(7.14159γt8a4)27.68953γt8a4×(0.66667γt8a4)212.00922γt8a4×(1.33333γt8a4)22(1.33333γt8a4)(7.14159γt8a4)×(0.66667γt8a4))]=0

Consider the value of K=Kγt8a4.

K338.1210K2+411.69009K744.47027=0

Solve the above Equation and get the value of K1=2.25890, K2=17.27274, and K3=19.08046.

The principal moment of inertia are K1=2.26γtga4, K2=17.27γtga4, and K3=19.08γtga4.

Thus, The principal moment of inertia are K1=2.26γtga4_, K2=17.27γtga4_, and K3=19.08γtga4_.

(b)

To determine

Find the angles made by the principal axis of inertia at O with the coordinate axis.

Sketch the body and show the orientation of the principal axis of inertia relative to x, y, and z axis.

(b)

Expert Solution
Check Mark

Answer to Problem 9.183P

The angles made by the principal axis of inertia at O with the coordinate axis is,

(θx)1=85°, (θy)1=36.8°, (θz)1=53.7°

(θx)2=81.7°, (θy)2=54.7°, (θz)1=143.4°

(θx)3=9.70°, (θy)3=99°, (θz)3=86.3°

Explanation of Solution

Given information:

Consider the direction cosines of each principal axis are denoted by λx,λy,λz.

Calculation:

Refer Part (a).

Consider K1.

Show the Equation 9.54 as follows:

(IxK1)(λx)1Ixy(λy)1Izx(λz)1=0Ixy(λx)1Iyz(λz)1+(IyK1)(λy)1=0} (1)

Substitute 18.91335γt8a4 for Ix, 7.68953γt8a4 for Iy, 1.33333γt8a4 for Ixy, 7.14159γt8a4 for Iyz, and 0.66667γt8a4 for Izx and 2.26γtga4 for K1.

(18.91335γt8a42.26γtga4)(λx)11.33333γt8a4(λy)10.66667γt8a4(λz)1=01.33333γt8a4(λx)17.14159γt8a4(λz)1+(7.68953γt8a42.26γtga4)(λy)1=0} (2)

Solve Equation (2).

Get the value of (λz)1=6.74653(λx)1,(λy)1=9.11761(λx)1.

Show the Equation 9.57 as follows:

(λx)12+(λy)12+(λz)12=1(λx)12+[9.11761(λx)1]2+[6.74653(λx)1]2=1

Solve above Equation and get the value of (λx)1=0.087825,(λy)1=0.80075,(λz)1=0.59251.

Show the direction cosines (θx)1,(θy)1,(θz)1 using the relation:

cos(θx)1=(λx)1=0.087825(θx)1=cos1(0.087825)=85°

cos(θz)1=(λz)1=0.59251(θz)1=cos1(0.59251)=53.7°

cos(θy)1=(λy)1=0.80075(θy)1=cos1(0.80075)=36.8°

Consider K2.

Show the Equation 9.54 as follows:

(IxK2)(λx)2Ixy(λy)2Izx(λz)2=0Ixy(λx)2Iyz(λz)2+(IyK2)(λy)2=0} (3)

Substitute 18.91335γt8a4 for Ix, 7.68953γt8a4 for Iy, 1.33333γt8a4 for Ixy, 7.14159γt8a4 for Iyz, and 0.66667γt8a4 for Izx and 17.27γtga4 for K2.

(18.91335γt8a417.27γtga4)(λx)21.33333γt8a4(λy)20.66667γt8a4(λz)2=01.33333γt8a4(λx)27.14159γt8a4(λz)2+(7.68953γt8a417.27γtga4)(λy)2=0} (4)

Solve Equation (4).

Get the value of (λz)2=5.58515(λx)2,(λy)2=4.02304(λx)2.

Show the Equation 9.57 as follows:

(λx)22+(λy)22+(λz)22=1(λx)22+[4.02304(λx)2]2+[5.58515(λx)2]2=1

Solve above Equation and get the value of (λx)2=0.14377,(λy)2=0.0.57839,(λz)2=0.80298.

Show the direction cosines (θx)2,(θy)2,(θz)2 using the relation:

cos(θx)2=(λx)2=0.14377(θx)2=cos1(0.14377)=81.7°

cos(θz)2=(λz)2=0.80298(θz)2=cos1(0.80298)=143.4°

cos(θy)2=(λy)2=0.0.57839(θy)2=cos1(0.0.57839)=54.7°

Consider K3.

Show the Equation 9.54 as follows:

(IxK3)(λx)3Ixy(λy)3Izx(λz)3=0Ixy(λx)3Iyz(λz)3+(IyK3)(λy)3=0} (5)

Substitute 18.91335γt8a4 for Ix, 7.68953γt8a4 for Iy, 1.33333γt8a4 for Ixy, 7.14159γt8a4 for Iyz, and 0.66667γt8a4 for Izx and 19.08γtga4 for K3.

(18.91335γt8a419.08γtga4)(λx)21.33333γt8a4(λy)20.66667γt8a4(λz)2=01.33333γt8a4(λx)27.14159γt8a4(λz)2+(7.68953γt8a419.08γtga4)(λy)2=0} (6)

Solve Equation (6).

Get the value of (λz)3=0.06522(λx)3,(λy)3=0.15794(λx)3.

Show the Equation 9.57 as follows:

(λx)32+(λy)32+(λz)32=1(λx)32+[0.15794(λx)3]2+[0.06522(λx)3]2=1

Solve above Equation and get the value of (λx)3=0.98571,(λy)3=0.15568,(λz)3=0.06429.

Show the direction cosines (θx)3,(θy)3,(θz)3 using the relation:

cos(θx)3=(λx)3=0.98571(θx)3=cos1(0.98571)=9.7°

cos(θz)3=(λz)3=0.06429(θz)3=cos1(0.06429)=86.3°

cos(θy)3=(λy)3=0.15568(θy)3=cos1(0.15568)=86.3°

The angles made by the principal axis of inertia at O with the coordinate axis is,

(θx)1=85°, (θy)1=36.8°, (θz)1=53.7°

(θx)2=81.7°, (θy)2=54.7°, (θz)1=143.4°

(θx)3=9.70°, (θy)3=99°, (θz)3=86.3°

Sketch the body and show the orientation of the principal axis of inertia relative to x, y, and z axis as shown in Figure 1.

Vector Mechanics for Engineers: Statics and Dynamics, Chapter 9.6, Problem 9.183P

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Chapter 9 Solutions

Vector Mechanics for Engineers: Statics and Dynamics

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