Vector Mechanics for Engineers: Dynamics
Vector Mechanics for Engineers: Dynamics
11th Edition
ISBN: 9780077687342
Author: Ferdinand P. Beer, E. Russell Johnston Jr., Phillip J. Cornwell, Brian Self
Publisher: McGraw-Hill Education
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Chapter 18, Problem 18.150RP

A uniform rod of mass m and length 5a is bent into the shape shown and is suspended from a wire attached at point B. Knowing that the rod is hit at point A in the negative y direction and denoting the corresponding impulse by ( F Δ t ) j , determine immediately after the impact (a) the velocity of the mass center G, (b) the angular velocity of the rod.

  Chapter 18, Problem 18.150RP, A uniform rod of mass m and length 5a is bent into the shape shown and is suspended from a wire

(a)

Expert Solution
Check Mark
To determine

The velocity of the mass centre G.

Answer to Problem 18.150RP

The velocity of the mass centre G is 0.

Explanation of Solution

Given information:

The mass of the rod is m, the length of the rod is 5a and the impulse in the y direction is (Δt)j.

The below figure represent the schematic diagram of the rod section.

Vector Mechanics for Engineers: Dynamics, Chapter 18, Problem 18.150RP

Figure-(1)

Write the expression of length of the section OA.

L1=L5       ...........(I)

Here, the total length of the rod is L.

Write the expression of length of the section AB.

L2=L5       ...........(II)

Write the expression of length of the section BC.

L3=L5       ...........(III)

Write the expression of length of the section CD.

L4=L5       ...........(IV)

Write the expression of length of the section DE.

L5=L5       ...........(V)

Write the expression of mass of the section OA.

m1=m5

Here, the total mass of the rod is L.

Write the expression of mass of the section AB.

m2=m5

Write the expression of mass of the section BC.

m3=m5

Write the expression of mass of the section CD.

m4=m5

Write the expression of mass of the section DE.

m5=m5

Write the expression of moment of inertia of section OA in x direction.

(Ix)1=m1L1212+m1L124+m1L124 ........ (VI)

Write the expression of moment of inertia of section OA in y direction.

(Iy)1=m1L1212+m1L12+m1L124 ........ (VII)

Write the expression of moment of inertia of section OA in z direction.

(Iz)1=m1L12+m1L124 ........ (VIII)

Write the expression of moment of inertia of section OA in xy direction.

(Ixy)1=m2L222 ........ (IX)

Write the expression of moment of inertia of section AB in x direction.

(Ix)2=m2L224 ........ (X)

Write the expression of moment of inertia of section AB in y direction.

(Iy)2=m2L223 ........ (XI)

Write the expression of moment of inertia of section AB in z direction.

(Iz)2=m2L2212+m2L224+m2L224 ........ (XII)

Write the expression of moment of inertia of section AB in xy direction.

(Ixy)2=m2L224 ........ (XIII)

Write the expression of moment of inertia of section BC in x direction.

(Ix)3=m3L324 ........ (XIV)

Write the expression of moment of inertia of section BC in x direction.

(Iy)3=0

Write the expression of moment of inertia of section BC in z direction.

(Iz)3=m3L3212 ........ (XV)

Write the expression of moment of inertia of section BC in xy direction.

(Ixy)3=0

Write the expression of moment of inertia of section CD in x direction.

(Ix)4=m4L424 ........ (XVI)

Write the expression of moment of inertia of section CD in y direction.

(Iy)4=m4L423 ........ (XVII)

Write the expression of moment of inertia of section CD in z direction.

(Iz)4=m4L4212+m4L424+m4L424 ........ (XVIII)

Write the expression of moment of inertia of section CD in xy direction.

(Ixy)4=m4L424 ........ (XIX)

Write the expression of moment of inertia of section DE in x direction.

(Ix)5=m5L5212+m5L524+m5L524 ........ (XX)

Write the expression of moment of inertia of section DE in y direction.

(Iy)5=m5L5212+m5L52+m5L524 ........ (XXI)

Write the expression of moment of inertia of section DE in z direction.

(Iz)5=m5L52+m5L524 ........ (XXII)

Write the expression of moment of inertia of section DE in xy direction.

(Ixy)5=m5L522 ........ (XXIII)

Write the expression of total moment of inertia in x direction.

Ix=(Ix)1+(Ix)2+(Ix)3+(Ix)4+(Ix)5 ........ (XXIV)

Write the expression of total moment of inertia in y direction.

Iy=(Iy)1+(Iy)2+(Iy)3+(Iy)4+(Iy)5 ........ (XXV)

Write the expression of total moment of inertia in z direction.

Iz=(Iz)1+(Iz)2+(Iz)3+(Iz)4+(Iz)5 ........ (XXVI)

Write the expression of total moment of inertia in xy direction.

Ixy=(Ixy)1+(Ixy)2+(Ixy)3+(Ixy)4+(Ixy)5 ........ (XXVII)

Write the expression of total moment of inertia in xz direction.

Ixz=(m1L122)+(m4L422)       ...........(XXVIII)

Write the expression of total moment of inertia in yz direction.

Iyz=(m2L224)+(m5L524)       ...........(XXIX)

Write the expression of angular momentum about x axis.

(HG)x=IxωxIxyωyIxzωz       ...........(XXX)

Write the expression of angular momentum about y axis.

(HG)y=IxyωxIyωyIyzωz       ...........(XXXI)

Write the expression of angular momentum about z axis.

(HG)z=IxzωxIyzωyIzωz       ...........(XXXII)

Write the expression of velocity of mass centre G.

V=I+(Δt)jm ........ (XXXIII)

Here, the force is F, the change in time is Δt, the total mass is m, the impact is I and the unit vector in y direction is j.

Calculation:

Substitute 5a for L in Equation (I).

L1=5a5=a

Substitute 5a for L in Equation (II).

L2=5a5=a

Substitute 5a for L in Equation (III).

L3=5a5=a

Substitute 5a for L in Equation (IV).

L4=5a5=a

Substitute 5a for L in Equation (V).

L5=5a5=a

Substitute m5 for m1, a for L1 in Equation (VI).

(Ix)1=m5a212+m5a24+m5a24=ma260+ma220+ma220=7ma260

Substitute m5 for m1, a for L1 in Equation (VII).

(Iy)1=m5a212+m5a2+m5a24=ma260+ma25+ma220=4ma215

Substitute m5 for m1, a for L1 in Equation (VIII).

(Iz)1=m5a2+m5a24=ma25+ma220=ma24

Substitute m5 for m2, a for L2 in Equation (IX).

(Ixy)1=m5a22=ma210

Substitute m5 for m2, a for L2 in Equation (X).

(Ix)2=m5a24=ma220

Substitute m5 for m2, a for L2 in Equation (XI).

(Iy)2=m5a23=ma215

Substitute m5 for m2, a for L2 in Equation (XII).

(Iz)2=m5a212+m5a24+m5a24=ma260+ma220+ma220=7ma260

Substitute m5 for m2, a for L2 in Equation (XIII).

(Ixy)2=m5a24=ma220

Substitute m5 for m3, a for L3 in Equation (XIV).

(Ix)3=m5a24=ma220

Substitute m5 for m3, a for L3 in Equation (XV).

(Iz)3=m5a212=ma260

Substitute m5 for m4, a for L4 in Equation (X).

(Ix)4=m5a24=ma220

Substitute m5 for m4, a for L4 in Equation (XVII).

(Iy)4=m5a23=ma215

Substitute m5 for m2, a for L2 in Equation (XVIII).

(Iz)4=m5a212+m5a24+m5a24=ma260+ma220+ma220=7ma260

Substitute m5 for m4, a for L4 in Equation (XIX).

(Ixy)4=m5a24=ma220

Substitute m5 for m5, a for L5 in Equation (XX).

(Ix)5=m5a212+m5a24+m5a24=ma260+ma220+ma220=7ma260

Substitute m5 for m5, a for L5 in Equation (XXI).

(Iy)5=m5a212+m5a2+m5a24=ma260+ma25+ma220=4ma215

Substitute m5 for m5, a for L5 in Equation (XXII).

(Iz)5=m5a2+m5a24=ma25+ma220=ma24

Substitute m5 for m5, a for L5 in Equation (XXIII).

(Ixy)5=m5a22=ma210

Substitute 7ma260 for (Ix)1, 7ma260 for (Ix)5, ma220 for (Ix)2, ma220 for (Ix)4, and ma220 for (Ix)3 in Equation (XXIV).

Ix=(7ma260)+(ma220)+(ma220)+(ma220)+(7ma260)=(0.23ma2)+(0.15ma2)=0.38ma2

Substitute 4ma215 for (Iy)1, ma215 for (Iy)2, 0 for (Iy)3, ma215 for (Iy)4 and 4ma215 for (Iy)5 in Equation (XXV).

Iy=(4ma215)+(ma215)+(0)+(ma215)+(4ma215)=(0.53ma2)+(0.13ma2)+0=0.68ma2

Substitute ma24 for (Iz)1, 7ma260 for (Iz)2, ma260 for (Iz)3, 7ma260 for (Iz)4 and ma24 for (Iz)5 in Equation (XXVI).

Iz=(ma24)+(7ma260)+(ma260)+(7ma260)+(ma24)=(0.5ma2)+(0.05ma2)=0.55ma2

Substitute ma210 for (Ixy)1, ma220 for (Ixy)2, 0 for (Ixy)3, ma220 for (Ixy)4 and ma210 for (Ixy)5 in Equation (XXVII).

Ixy=(ma210)+(ma220)+(0)+(ma220)+(ma210)=(0.1ma2)(0.05ma2)(0.05ma2)(0.1ma2)=0.2ma20.1ma2=0.3ma2

Substitute m5 for m1, m5 for m4, a for L1 and a for L2 in Equation (XXVIII).

Ixz=(m5a22)+(m5a22)=ma210+ma210=0.2ma2

Substitute m5 for m2, m5 for m5, a for L2 and a for L5 in Equation (XXIX).

Iyz=(m5)a24(m5)a24=ma220ma220=0.1ma2

Substitute 0.38ma2 for Ix, 0.3ma2 for Ixy and 0.2ma2 for Ixz in Equation (XXX).

(HG)x=(0.38ma2)ωx(0.3ma2)ωy(0.2ma2)ωz=0.38ma2ωx+0.3ma2ωy0.2ma2ωz       ...........(XXXIII)

Substitute 0.3ma2 for Ixy, 0.68ma2 for Iy and 0.1ma2 for Iyz in Equation (XXXI)

(HG)y=(0.3ma2)ωx(0.68ma2)ωy(0.1ma2)ωz=0.3ma2ωx0.68ma2ωy+0.1ma2ωz       ...........(XXXIV)

Substitute 0.2ma2 for Ixz, 0.1ma2 for Iyz and 0.55ma2 for Iz in Equation (XXXII)

(HG)z=(0.2ma2)ωx(0.1ma2)ωy(0.55ma2)ωz=0.2ma2ωx+0.1ma2ωy0.55ma2ωz       ...........(XXXV)

Substitute (Δt)j for I in Equation (XXXIII).

V=(Δt)j+(Δt)jm=0m=0

Conclusion:

The velocity of the mass centre G is 0.

Expert Solution
Check Mark
To determine

(b)

The angular velocity of the rod.

Answer to Problem 18.150RP

The angular velocity of the rod is Δtma(2.5i1.45j+2.2k).

Explanation of Solution

Given information:

Write the expression of angular momentum in z direction.

(HG)z=L1I .      ...........(XXXVI)

Write the expression of angular velocity of the rod.

ω=(ωx)i+(ωy)j+(ωz)k       ...........(XXXVII)

Here, the angular velocity in x direction is ωx, the angular velocity in y direction is ωy and the angular velocity in z direction is ωz.

Calculation:

Substitute (Δt) for I and a for L1 in Equation (XXXVI).

(HG)z=a((Δt))=a(Δt)

Substitute 0 for (HG)x in Equation (XXXIII).

0=0.38ma2ωx+0.3ma2ωy0.2ma2ωz       ...........(XXXVIII)

Substitute 0 for (HG)y in Equation (XXXIV).

0=0.3ma2ωx0.68ma2ωy+0.1ma2ωz       ...........(XXXIX)

Substitute a(Δt) for (HG)z in Equation (XXXV).

a(Δt)=0.2ma2ωx+0.1ma2ωy0.55ma2ωz       ...........(XXXX)

Solve Equation (XXXIII), (XXXIX) and (XXXX).

ωx=2.5FΔtma

ωy=1.45FΔtma

ωz=2.2FΔtma

Substitute 2.5FΔtma for ωx, 1.45FΔtma for ωy and 2.2FΔtma for ωz in Equation (XXXVII).

ω=(2.5FΔtma)i+(1.45FΔtma)j+(2.2FΔtma)k=Δtma(2.5i1.45j+2.2k)

Conclusion:

The angular velocity of the rod is Δtma(2.5i1.45j+2.2k).

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Chapter 18 Solutions

Vector Mechanics for Engineers: Dynamics

Ch. 18.1 - Prob. 18.11PCh. 18.1 - Prob. 18.12PCh. 18.1 - Prob. 18.13PCh. 18.1 - Prob. 18.14PCh. 18.1 - Prob. 18.15PCh. 18.1 - For the assembly of Prob. 18.15, determine (a) the...Ch. 18.1 - Prob. 18.17PCh. 18.1 - Determine the angular momentum of the shaft of...Ch. 18.1 - Prob. 18.19PCh. 18.1 - Prob. 18.20PCh. 18.1 - Prob. 18.21PCh. 18.1 - Prob. 18.22PCh. 18.1 - Prob. 18.23PCh. 18.1 - Prob. 18.24PCh. 18.1 - Prob. 18.25PCh. 18.1 - Prob. 18.26PCh. 18.1 - Prob. 18.27PCh. 18.1 - Prob. 18.28PCh. 18.1 - Prob. 18.29PCh. 18.1 - Prob. 18.30PCh. 18.1 - Prob. 18.31PCh. 18.1 - Prob. 18.32PCh. 18.1 - Prob. 18.33PCh. 18.1 - Prob. 18.34PCh. 18.1 - Prob. 18.35PCh. 18.1 - Prob. 18.36PCh. 18.1 - Prob. 18.37PCh. 18.1 - Prob. 18.38PCh. 18.1 - Prob. 18.39PCh. 18.1 - Prob. 18.40PCh. 18.1 - Prob. 18.41PCh. 18.1 - Prob. 18.42PCh. 18.1 - Determine the kinetic energy of the disk of Prob....Ch. 18.1 - Prob. 18.44PCh. 18.1 - Prob. 18.45PCh. 18.1 - Prob. 18.46PCh. 18.1 - Prob. 18.47PCh. 18.1 - Prob. 18.48PCh. 18.1 - Prob. 18.49PCh. 18.1 - Prob. 18.50PCh. 18.1 - Prob. 18.51PCh. 18.1 - Prob. 18.52PCh. 18.1 - Determine the kinetic energy of the space probe of...Ch. 18.1 - Prob. 18.54PCh. 18.2 - Determine the rate of change H.G of the angular...Ch. 18.2 - Prob. 18.56PCh. 18.2 - Prob. 18.57PCh. 18.2 - Prob. 18.58PCh. 18.2 - Prob. 18.59PCh. 18.2 - Prob. 18.60PCh. 18.2 - Prob. 18.61PCh. 18.2 - Prob. 18.62PCh. 18.2 - Prob. 18.63PCh. 18.2 - Prob. 18.64PCh. 18.2 - A slender, uniform rod AB of mass m and a vertical...Ch. 18.2 - A thin, homogeneous triangular plate of weight 10...Ch. 18.2 - Prob. 18.67PCh. 18.2 - Prob. 18.68PCh. 18.2 - Prob. 18.69PCh. 18.2 - Prob. 18.70PCh. 18.2 - Prob. 18.71PCh. 18.2 - Prob. 18.72PCh. 18.2 - Prob. 18.73PCh. 18.2 - Prob. 18.74PCh. 18.2 - Prob. 18.75PCh. 18.2 - Prob. 18.76PCh. 18.2 - Prob. 18.77PCh. 18.2 - Prob. 18.78PCh. 18.2 - Prob. 18.79PCh. 18.2 - Prob. 18.80PCh. 18.2 - Prob. 18.81PCh. 18.2 - Prob. 18.82PCh. 18.2 - Prob. 18.83PCh. 18.2 - Prob. 18.84PCh. 18.2 - Prob. 18.85PCh. 18.2 - Prob. 18.86PCh. 18.2 - Prob. 18.87PCh. 18.2 - Prob. 18.88PCh. 18.2 - Prob. 18.89PCh. 18.2 - The slender rod AB is attached by a clevis to arm...Ch. 18.2 - The slender rod AB is attached by a clevis to arm...Ch. 18.2 - Prob. 18.92PCh. 18.2 - The 10-oz disk shown spins at the rate 1=750 rpm,...Ch. 18.2 - Prob. 18.94PCh. 18.2 - Prob. 18.95PCh. 18.2 - Prob. 18.96PCh. 18.2 - Prob. 18.97PCh. 18.2 - Prob. 18.98PCh. 18.2 - Prob. 18.99PCh. 18.2 - Prob. 18.100PCh. 18.2 - Prob. 18.101PCh. 18.2 - Prob. 18.102PCh. 18.2 - Prob. 18.103PCh. 18.2 - A 2.5-kg homogeneous disk of radius 80 mm rotates...Ch. 18.2 - For the disk of Prob. 18.99, determine (a) the...Ch. 18.2 - Prob. 18.106PCh. 18.3 - Prob. 18.107PCh. 18.3 - A uniform thin disk with a 6-in. diameter is...Ch. 18.3 - Prob. 18.109PCh. 18.3 - Prob. 18.110PCh. 18.3 - Prob. 18.111PCh. 18.3 - Prob. 18.112PCh. 18.3 - Prob. 18.113PCh. 18.3 - Prob. 18.114PCh. 18.3 - Prob. 18.115PCh. 18.3 - Prob. 18.116PCh. 18.3 - Prob. 18.117PCh. 18.3 - Prob. 18.118PCh. 18.3 - Show that for an axisymmetric body under no force,...Ch. 18.3 - Prob. 18.120PCh. 18.3 - Prob. 18.121PCh. 18.3 - Prob. 18.122PCh. 18.3 - Using the relation given in Prob. 18.121,...Ch. 18.3 - Prob. 18.124PCh. 18.3 - Prob. 18.125PCh. 18.3 - Prob. 18.126PCh. 18.3 - Prob. 18.127PCh. 18.3 - Prob. 18.128PCh. 18.3 - An 800-lb geostationary satellite is spinning with...Ch. 18.3 - Solve Prob. 18.129, assuming that the meteorite...Ch. 18.3 - Prob. 18.131PCh. 18.3 - Prob. 18.132PCh. 18.3 - Prob. 18.133PCh. 18.3 - Prob. 18.134PCh. 18.3 - Prob. 18.135PCh. 18.3 - Prob. 18.136PCh. 18.3 - Prob. 18.137PCh. 18.3 - Prob. 18.138PCh. 18.3 - Prob. 18.139PCh. 18.3 - Prob. 18.140PCh. 18.3 - Prob. 18.141PCh. 18.3 - Prob. 18.142PCh. 18.3 - Prob. 18.143PCh. 18.3 - Prob. 18.144PCh. 18.3 - Prob. 18.145PCh. 18.3 - Prob. 18.146PCh. 18 - Prob. 18.147RPCh. 18 - Prob. 18.148RPCh. 18 - A rod of uniform cross-section is used to form the...Ch. 18 - A uniform rod of mass m and length 5a is bent into...Ch. 18 - Prob. 18.151RPCh. 18 - Prob. 18.152RPCh. 18 - A homogeneous disk of weight W=6 lb rotates at the...Ch. 18 - Prob. 18.154RPCh. 18 - Prob. 18.155RPCh. 18 - Prob. 18.156RPCh. 18 - Prob. 18.157RPCh. 18 - Prob. 18.158RP
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