Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)
10th Edition
ISBN: 9780073398204
Author: Richard G Budynas, Keith J Nisbett
Publisher: McGraw-Hill Education
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Textbook Question
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Chapter 3, Problem 48P

3–48 and 3–49 The beam shown is loaded in the xy and xz planes.

  1. (a) Find the y- and z-components of the reactions at the supports.
  2. (b) Plot the shear-force and bending-moment diagrams for the xy and xz planes. Label the diagrams properly and provide the values at key points.
  3. (c) Determine the net shear-force and bending-moment at the key points of part (b).
  4. (d) Determine the maximum tensile bending stress. For Prob. 3–48, use the cross section given in Prob. 3–34, part (a). For Prob. 3–49, use the cross section given in Prob. 3–39, part (b).

Chapter 3, Problem 48P, 348 and 349 The beam shown is loaded in the xy and xz planes. (a) Find the y- and z-components of

(a)

Expert Solution
Check Mark
To determine

The y-components of the reactions at the supports of the beam.

The z-components of the reactions at the supports of the beam.

Answer to Problem 48P

The y-components of the reactions at the supports O and of the beam are 0.649kN and 1.949kN respectively.

The z-components of the reactions at the supports O and C of the beam are 1.625kN and 1.375kN respectively.

Explanation of Solution

The following figure shows the forces acting on the beam along x-z plane.

Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering), Chapter 3, Problem 48P , additional homework tip  1

Figure-(1)

Write the equilibrium equation of force applied on the beam in z-direction.

    Fz=0R1z(1.5kN)(2(sin30°)kN/m)(1.5m)+R2z=0R1z+R2z3kN=0R1z+R2z=3kN                                     (I)

Write the bending moment at the support O in x-z plane.

    MO=0[(1.5kN)(0.5m)+(2(sin30°)kN/m)(1.5m)(0.5m+1m+1.5m2)R2z(3m)]=0(0.75kNm)+(1.5kN)(2.25m)R2z(3m)=0 (II)

The following figure shows the forces acting on the beam along x-y plane.

Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering), Chapter 3, Problem 48P , additional homework tip  2

Figure-(2)

Write the equilibrium equation of force applied on the beam in y-direction.

    Fy=0R1y(2cos(30°)kN/m)(1.5m)+R2y=0R1y+R2y2.598kN=0R1y+R2y=2.598kN                                                 (III)

Write the bending moment at the support O in x-y plane.

    MO=0(2cos(30°)kN/m)(1.5m)(0.5m+1m+1.5m2)+R2y(3m)=0(2.598kN)(2.25m)+R2y(3m)=0          (IV)

Conclusion:

From Equation (II), R2z=1.375kN.

Substitute 1.375kN for R2z in Equation (I).

    R1z+1.375kN=3kNR1z=(3kN)(1.375kN)R1z=1.625kN

Thus, the z-components of the reactions at the supports O and C of the beam are 1.625kN and 1.375kN respectively.

Simplify Equation (IV).

    (2.598kN)(2.25m)+R2y(3m)=0R2y=5.8455kNm3R2y1.949kN

Substitute 1.949kN for R2y in Equation (III).

    R1y+1.949kN=2.598kNR1y=(2.598kN)(1.949kN)R1y=0.649kN

Thus, the y-components of the reactions at the supports O and of the beam are 0.649kN and 1.949kN respectively.

(b)

Expert Solution
Check Mark
To determine

The shear force and bending moment diagram of the beam.

Explanation of Solution

Write the expression for the moment at point A.

    MAz=R2z(2.5m)+(2sin30°kN/m)(1.5m)(1.5m2+1m)        (V)

Write the expression for the moment at point B.

    MBz=R2z(1.5m)+(2sin30°kN/m)(1.5m)(1.5m2)                 (VI)

Write the equation for the shear force.

    Vz=2sin30°x+R2z                                                                     (VII)

Write the expression for the maximum bending moment.

    Mzmax=R2z(x)+(2sin30°kN/m)(x)(x2)                                 (VIII)

Write the expression for the bending moment at B.

    MBy=R2y(1.5m)(2cos30°kN/m)(1.5m)(1.5m2)                    (IX)

Write the equation for the shear force.

    Vy=2cos30°xR2y                                                                          (X)

Write the expression for the maximum bending moment.

    Mymax=R2y(x)(2cos30°kN/m)(x)(x2)                                     (XI)

Conclusion:

Substitute 1.375kN for R2z in Equation (V).

    MAz=(1.375kN)(2.5m)+(2sin30°kN/m)(1.5m)(1.5m2+1m)=(1.375kN)(2.5m)+(1kN/m)(1.5m)(1.75m)=0.8125kNm

Substitute 1.375kN for R2z in Equation (VI).

    MBz=(1.375kN)(1.5m)+(2sin30°kN/m)(1.5m)(1.5m2)=(1.375kN)(1.5m)+(1kN/m)(1.5m)(0.75m)=0.9375kNm

The maximum bending moment occur at Vz=0kN.

Substitute 0kN for Vz, and 1.375kN for R2z in Equation (VII).

    0kN=2sin30°x+1.375kN0kN=xkN/m+1.375kNx=1.375m

Substitute 1.375m for x, and 1.375kN for R2z in Equation (VIII).

    Mzmax=(1.375kN)(1.375m)+(2sin30°kN/m)(1.375m)(1.375m2)=(1.375kN)(1.375m)+(1kN/m)(1.375m)(1.375m2)=0.9453kNm

The following figure shows the shear force and bending moment diagram of the beam along x-z plane.

Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering), Chapter 3, Problem 48P , additional homework tip  3

Figure-(3)

Substitute 1.949kN for R2y in Equation (IX).

    MBy=(1.949kN)(1.5m)(2cos30°kN/m)(1.5m)(1.5m2)=(1.949kN)(1.5m)(1.732kN/m)(1.5m)(0.75m)=0.975kNm

The maximum bending moment occur at Vy=0kN.

Substitute 0kN for Vy, and 1.949kN for R2y in Equation (X).

    0kN=2cos30°x1.949kN0kN=1.732xkN/m1.949kNx=1.125m

Substitute 1.125m for x, and 1.949kN for R2y in Equation (XI).

    Mymax=1.949kN(1.125m)(2cos30°kN/m)(1.125m)(1.125m2)=1.949kN(1.125m)(1.732kN/m)(1.125m)(0.5625m)=1.096kNm

The following figure shows the shear force and bending moment diagram of the beam along x-y plane.

Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering), Chapter 3, Problem 48P , additional homework tip  4

Figure-(4)

(c)

Expert Solution
Check Mark
To determine

The net bending moment at x=3m.

The net shear force at x=3m.

The net bending moment at x=1.5m.

The net shear force at x=1.5m.

The net bending moment at x=0.5m.

The net shear force at x=0.5m.

The net bending moment at x=0m.

The net shear force at x=0m.

Answer to Problem 48P

The net bending moment at x=3m is 0kNm.

The net shear force at x=3m is 2.385kN.

The net bending moment at x=1.5m is 1.352kNm.

The net shear force at x=1.5m is 0.661kN.

The net bending moment at x=0.5m is 0.8749kNm.

The net shear force at x=0.5m is 1.749kN.

The net bending moment at x=0m is 0kNm.

The net shear force at x=0m is 1.749kN.

Explanation of Solution

Write the expression for the net shear force on the beam.

    V=Vz2+Vy2                                                                        (XII)

Write the expression for the net bending moment on the beam.

    M=Mz2+My2                                                                  (XIII)

Conclusion:

The following table shows the magnitudes of bending moment and shear force along x-y and x-z plane from the shear force and bending moment diagram.

x(m)Vz(kN)Vy(kN)My(kNm)Mz(kNm)
01.6250.649100
0.51.6250.64910.81250.3246
1.50.1250.64910.93750.9737
31.3751.94900

At x=0m:

Substitute 1.625kN for Vz, and 0.6491kN for Vy in Equation (XII).

    V0=(1.625kN)2+(0.6491kN)2=2.640625+0.42133kN=1.749kN

Thus, the net shear force at x=0m is 1.749kN.

Substitute 0kNm for Mz, and 0kNm for My in Equation (XIII).

    M0=(0kNm)2+(0kNm)2=0kNm

Thus, the net bending moment at x=0m is 0kNm.

At x=0.5m:

Substitute 1.625kN for Vz, and 0.6491kN for Vy in Equation (XII).

    V0.5=(1.625kN)2+(0.6491kN)2=2.640625+0.42133kN=1.749kN

Thus, the net shear force at x=0.5m is 1.749kN.

Substitute 0.8125kNm for Mz, and 0.3246kNm for My in Equation (XIII).

    M0.5=(0.8125kNm)2+(0.3246kNm)2=(0.66015+0.10536)kN2m2=0.8749kNm

Thus, the net bending moment at x=0.5m is 0.8749kNm.

At x=1.5m:

Substitute 0.125kN for Vz, and 0.6491kN for Vy in Equation (XII).

    V1.5=(0.125kN)2+(0.6491kN)2=0.015625+0.42133kN=0.661kN

Thus, the net shear force at x=1.5m is 0.661kN.

Substitute 0.9737kNm for Mz, and 0.9375kNm for My in Equation (XIII).

    M1.5=(0.9737kNm)2+(0.9375kNm)2=1.82699kNm=1.352kNm

Thus, the net bending moment at x=1.5m is 1.352kNm.

At x=3m:

Substitute 1.375kN for Vz, and 1.949kN for Vy in Equation (XII).

    V3=(1.375kN)2+(1.949kN)2=1.890625+3.798601kN=2.385kN

Thus, the net shear force at x=3m is 2.385kN.

Substitute 0kNm for Mz, and 0kNm for My in Equation (XIII).

    M3=(0kNm)2+(0kNm)2=0kNm

Thus, the net bending moment at x=3m is 0kNm.

(d)

Expert Solution
Check Mark
To determine

The maximum tensile bending stress on the beam.

Answer to Problem 48P

The maximum tensile bending stress on the beam is 73.52MPa.

Explanation of Solution

The following diagram shows the cross-section of the beam.

Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering), Chapter 3, Problem 48P , additional homework tip  5

Figure-(5)

Write the expression for the second moment of area of the section about z-axis.

  Iz=Ia2Ib                                                                       (XIV)

Here, the second moment area of the area a is Ia and the second moment of area of the area b is Ib.

Write the moment of inertia of the rectangular section.

    I=BH312                                                                               (XV)

Here total height of the section is H, and the width is H.

Write the expression for the moment of inertia about y-axis.

    Iy=2(hB312)+h2b2312                                                             (XVI)

Here, the height of the flange is h, height of the web is h2, and the width is b2.

Write the expression for maximum tensile bending stress.

    σmax=MzyAIz+MyzAIy                                                       (XVII)

Conclusion:

Substitute 40mm for B and 75mm for H in Equation (XV).

    Ia=(40mm)(75mm)312=1406250mm4

Substitute 34mm for B and 25mm for H in Equation (XV).

    Ib=(34mm)(25mm)312=44270.83mm4

Substitute 1406250mm4 for Ia and 44270.83mm4 for Ib in Equation (XIV).

    Iz=1406250mm42×44270.83mm4=(1317708.34mm4)(1012m41mm4)1.32×106m4

Substitute 40mm for B, 25mm for h, 25mm for h2, and 6mm for b2 in Equation (XVI).

    Iy=2((25mm)(40mm)312)+(25mm)(6mm)312=2(133333.33mm4)+450mm4=(267116.66mm4)(1012m41mm4)2.67×107m4

Substitute 1.075kNm for Mz, 0.9408kNm for My, 37.5mm for yA, 20mm for zA, 1.32×106m4 for Iz, and 2.67×107m4 for Iy in Equation (XVII).

    σmax=(1.075kNm)(37.5mm)1.32×106m4+(0.9408kNm)(20mm)2.67×107m4=[(1.075kNm)(37.5mm)(1m1000mm)1.32×106m4+(0.9408kNm)(20mm)(1m1000mm)2.67×107m4]=[3.0539×103kN/m2+7.0471×104kN/m2](1MPa103kN/m2)=73.52MPa

Thus, the maximum tensile bending stress on the beam is 73.52MPa.

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Chapter 3 Solutions

Shigley's Mechanical Engineering Design (McGraw-Hill Series in Mechanical Engineering)

Ch. 3 - Repeat Prob. 37 using singularity functions...Ch. 3 - Repeat Prob. 38 using singularity functions...Ch. 3 - For a beam from Table A9, as specified by your...Ch. 3 - A beam carrying a uniform load is simply supported...Ch. 3 - For each of the plane stress states listed below,...Ch. 3 - Repeat Prob. 315 for: (a)x = 28 MPa, y = 7 MPa, xy...Ch. 3 - Repeat Prob. 315 for: a) x = 12 kpsi, y = 6 kpsi,...Ch. 3 - For each of the stress states listed below, find...Ch. 3 - Repeat Prob. 318 for: (a)x = 10 kpsi, y = 4 kpsi...Ch. 3 - The state of stress at a point is x = 6, y = 18, z...Ch. 3 - The state of stress at a point is x = 6, y = 18, z...Ch. 3 - Repeat Prob. 320 with x = 10, y = 40, z = 40, xy =...Ch. 3 - A 34-in-diameter steel tension rod is 5 ft long...Ch. 3 - Repeat Prob. 323 except change the rod to aluminum...Ch. 3 - A 30-mm-diameter copper rod is 1 m long with a...Ch. 3 - A diagonal aluminum alloy tension rod of diameter...Ch. 3 - Repeat Prob. 326 with d = 16 mm, l = 3 m, and...Ch. 3 - Repeat Prob. 326 with d = 58 in, l = 10 ft, and...Ch. 3 - Electrical strain gauges were applied to a notched...Ch. 3 - Repeat Prob. 329 for a material of aluminum. 3-29...Ch. 3 - The Roman method for addressing uncertainty in...Ch. 3 - Using our experience with concentrated loading on...Ch. 3 - The Chicago North Shore Milwaukee Railroad was an...Ch. 3 - For each section illustrated, find the second...Ch. 3 - 3-35 to 3-38 For the beam illustrated in the...Ch. 3 - 3-35 to 3-38 For the beam illustrated in the...Ch. 3 - 3-35 to 3-38 For the beam illustrated in the...Ch. 3 - 3-35 to 3-38 For the beam illustrated in the...Ch. 3 - The figure illustrates a number of beam sections....Ch. 3 - A pin in a knuckle joint canning a tensile load F...Ch. 3 - Repeat Prob. 3-40 for a = 6 mm, b = 18 mm. d = 12...Ch. 3 - For the knuckle joint described in Prob. 3-40,...Ch. 3 - The figure illustrates a pin tightly fitted into a...Ch. 3 - For the beam shown, determine (a) the maximum...Ch. 3 - A cantilever beam with a 1-in-diameter round cross...Ch. 3 - Consider a simply supported beam of rectangular...Ch. 3 - In Prob. 346, h 0 as x 0, which cannot occur. 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