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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Chapter 6, Problem 27P

An M14 × 2 hex-head bolt with a nut is used to clamp together two 20-mm steel plates. Compare the results of finding the overall member stiffness by use of Eqs. (8-20), (8-22), and (8-23).

6-27 Using the modified Goodman criterion for infinite life, repeat Prob. 6-25 for each of the following loading conditions:

  1. (a)   0 kN to 28 kN
  2. (b)   12 kN to 28 kN
  3. (c)   −28 kN to 12 kN

(a)

Expert Solution
Check Mark
To determine

The yield factor of safety.

The fatigue factor of safety using Goodman criterion.

The number of cycle to failure.

Answer to Problem 27P

The yield factor of safety is 3.32.

The fatigue factor of safety using Goodman criterion 0.95.

The number of cycle to failure is 586000cycles.

Explanation of Solution

Write the expression of endurance limit.

Se=0.5Sut (I)

Here, endurance limit is Se, and the minimum tensile strength of material is Sut.

Write the expression for surface modification factor.

ka=aSutb (II)

Here, surface modification factor is ka and the constants are a and b.

Write the expression for endurance limit at critical location of a machine part in the geometry.

Se=kakbkcSe'.                               (III)

Here, the endurance limit at critical location is Se, the surface modification factor is ka, the size modification factor is kb, the load modification factor is kc.

Write the expression for fatigue stress concentration factor.

Kf=1+q(Kt1) (IV)

Here, the fatigue stress concentration is factor is Kf, the notch sensitivity factor is q and theoretical stress concentration factor is the Kt.

Write the expression for area of the steel bar at the hole or the minimum cross section area on which load is acting.

A=(wd)h (V)

Here, width of the bar is w, diameter of hole is d and thickness of bar is h.

Write the expression for the maximum stress.

σ(max)=FmaxA (VI)

Here, the maximum force acting on the bar is Fmax and maximum stress produced in the bar is σmax.

Write the expression for the minimum stress.

σmin=FminA (VII)

Here, the minimum force acting on the bar is Fmin and minimum stress acting on the bar is σmin.

Write the expression for the nominal amplitude stress.

σao=|σmaxσmin2| (VIII)

Here, the nominal amplitude stress is σao.

Write the expression for the nominal midrange stress.

σmo=|σmax+σmin2| (IX)

Here, the nominal amplitude stress for is σmo.

Write the expression for the amplitude component.

σa=Kf×σao (X)

Here, the amplitude component is σa and the above expression is valid when notch present in the component.

Write the expression for the midrange component.

σm=Kf×σmo . (XI)

Here, the midrange component is σm.

The Equation (XI) is valid when notch is present in the component.

Write the Expression for the yield factor of safety.

ny=|Syσmax| (XII)

Here, the yield factor of safety is ny and the yield strength is Sy.

Write the expression for the fatigue factor of safety using the modified Goodman criterion.

(nf)G=1σaSe+σmSut (XIII)

Write the expression for the completely reversed stress.

σrev=σa1σmSut (XIV)

Here, the fatigue factor of safety using Goodman criterion is (nf)G.

Write the expression of number of cycle in case of completely reversed stress.

N=(σreva)1/b . (XV)

Here, the number of cycle are N, completely reversed stress is σrev, constants are a and b.

Write the expression for the constant a.

a=(fSut)2Se (XVI)

Here, the strength fraction is f.

Write the expression for the constant b.

b=13log(fSutSe) (XVII)

Conclusion:

Substitute 590 MPa for SUT in Equation (I).

Se=0.5×590MPa=295MPa

Refer to Table 6-2 “Parameter of Marin surface modification factor” to obtain the constant a as 0.451 and the constant b as 0.265.

Substitute 4.51 for a and 0.265 for b in Equation (II).

ka=4.51×(590MPa)0.265=0.832

Refer to equation 621 to obtain kb as 1 and equation 626 to obtain the kc as 0.85.

Substitute 0.897 for Ka, 1 for kb and 0.85 for kc in Equation (III).

Se=0.832×1×0.85×(295MPa)=208.6MPa

Refer to fig 620 “Notch sensitivity chart for materials” the value of q is 0.83 and refer to fig A-15-1 “The bar in simple tension or compression with transverse hole” at d/w=0.24 the value of theoretical stress concentration factor is 2.44.

Substitute 2.44 for kt and 0.83 for q in Equation (IV)

Kf=1+0.83×(2.441)=2.1952.20

Substitute 25mm for w and 10mm for h in Equation (V).

A=(25mm6mm)(10mm)=(19mm)(10mm)=190mm2

Substitute 28kN for Fmax and 190mm2 for A in Equation (VI).

σmax=28kN190mm2=0.14737(kN/mm2)(1000N1kN)=0.14737(kN/mm2)(1000N1kN)(1MPa1N/mm2)=147.4MPa

Substitute 0kN for Fmin and 190mm2 for A in Equation (VII).

σmin=0kN190mm2=0(kN/mm2)(1000N1kN)=0(kN/mm2)(1000N1kN)(1MPa1N/mm2)=0MPa

Substitute 147.4MPa for σmax and 0MPa for σmin in Equation (VIII).

σao=|(147.4MPa)(0MPa)2|=147.4MPa2=73.7MPa

Substitute 147.4MPa for σmax and 147.4MPa for σmin in Equation (IX).

σmo=|(147.4MPa)+(0MPa)2|=147.4MPa2=73.7MPa

Substitute 73.7MPa for σao and 2.20 for Kf in Equation (X).

σa=2.20×(73.7MPa)=162.1MPa

Substitute 73.7MPa for σmo and 2.20 for Kf in Equation (XI).

σm=2.20×(73.7MPa)=162.1MPa

Substitute 490MPa for Sy and 147.4MPa for σmax in Equation (XII).

ny=|490MPa147.4MPa|=3.32

Thus, the yield factor of safety is 3.32.

Substitute 208.6MPa for Se, 162.1MPa for σa, 162.1MPa for σm, and 590MPa for Sut in Equation (XIII).

(nf)G=1162.1MPa208.6MPa+162.1MPa590MPa=10.777+0.2747=0.95

Thus, the fatigue factor of safety using Goodman criterion is 0.95.

Substitute 162.1MPa for σa, 162.1MPa for σm, and 590MPa for Sut in Equation (XIV).

σrev=162.1MPa1162.1MPa590MPa=162.1MPa0.7252=223.5MPa

From fig-618 “fatigue strength fraction f of Sut at 103 cycles for Se and S'e at 106 cycles” the value of f is 0.87.

Substitute 0.87 for f, 590MPa and 208.6MPa for Se in Equation (XVI).

a=((0.87)(590MPa))2208.6MPa=263476.89208.6MPa=1263.07MPa1263.07MPa

Substitute 0.87 for f, 590MPa for Sut and 208.6MPa for Se in Equation (XVII).

b=13log((0.87)(590MPa)208.6MPa)=13log(2.4606)=13(0.39105)=0.1304

Substitute 1263MPa for a, 0.1304 for b, and 223.5 for σrev in Equation (XV).

N=(223.5MPa1263MPa)1/0.1304=(0.17695)1/0.1304=585916.9cycles586000cycles

Thus, the number of cycle to failure is 586000cycles.

(b)

Expert Solution
Check Mark
To determine

The Yield factor of safety.

The fatigue factor of safety using Goodman criterion.

Answer to Problem 27P

The yield factor of safety is 3.32.

The fatigue factor of safety is 1.2.

Explanation of Solution

Write the expression of maximum stress.

σ(max)=FmaxA (XVIII)

Here, the maximum force acting on the bar is Fmax and maximum stress produced in the bar is σmax.

Write the expression of minimum stress.

σmin=FminA (XIX)

Here, the minimum force acting on the bar is Fmin and minimum stress acting on the bar is σmin.

Write the expression of nominal amplitude stress.

σao=|σmaxσmin2| (XX)

Here, the nominal amplitude stress is σao.

Write the expression of nominal midrange stress.

σmo=|σmax+σmin2| (XXI)

Here, the nominal amplitude stress for is σmo.

Write the expression of amplitude component.

σa=Kf×σao (XXII)

Here, the amplitude component is σa and the above expression is valid when notch present in the component.

Write the expression of midrange component.

σm=Kf×σmo . (XXIII)

Here, the midrange component is σm and the above expression is valid when notch present in the component.

Write the Expression of yield factor of safety.

ny=|Syσmax| (XXIV)

Here, the yield factor of safety is ny and the yield strength is Sy.

Write the expression of fatigue factor of safety using the modified Goodman criterion.

(nf)G=1σaSe+σmSut (XXV)

Conclusion:

Substitute 28kN for Fmax and 190mm2 for A in Equation (XVIII)

σmax=28kN190mm2=0.14737(kN/mm2)(1000N1kN)=0.14737(kN/mm2)(1000N1kN)(1MPa1N/mm2)=147.4MPa

Substitute 12kN for Fmin and 190mm2 for A in Equation (XIX).

σmin=12kN190mm2=0.0632(kN/mm2)(1000N1kN)=0.0632(kN/mm2)(1000N1kN)(1MPa1N/mm2)=63.2MPa

Substitute 147.4MPa for σmax and 63.2MPa for σmin in Equation (XX).

σao=|(147.4MPa)(63.2MPa)2|=84.2MPa2=42.1MPa

Substitute 147.4MPa for σmax and 63.2MPa for σmin in Equation (XXI).

σmo=|(147.4MPa)+(63.2MPa)2|=210.6MPa2=105.3MPa

Substitute 42.1MPa for σao and 2.20 for Kf in Equation (XXI).

σa=2.20×42.1MPa=92.83MPa

Substitute 105.3MPa for σmo and 2.20 for Kf in Equation (XXIII).

σm=2.20×105.3MPa=231.7MPa

Substitute 490MPa for Sy and 147.4MPa for σmax in Equation (XXIV).

ny=|490MPa147.4MPa|=3.32

Thus, the yield factor of safety is 3.32.

Substitute 208.6MPa for Se, 92.83MPa for σa, 231.7MPa for σm, and 590MPa for Sut in Equation (XXV)

(nf)G=192.83MPa208.6MPa+231.5MPa590MPa=10.83738=1.1941.2

Thus, the fatigue factor of safety using Goodman criterion is 1.2.

(c)

Expert Solution
Check Mark
To determine

Yield factor of safety.

The fatigue factor of safety using Goodman criterion.

Number of cycle to failure.

Answer to Problem 27P

The yield factor of safety is 3.32.

The fatigue factor of safety is 0.905.

The number of cycle to failure is 446000cycles.

Explanation of Solution

Write the expression of maximum stress.

σ(max)=FmaxA (XXVI)

Here, the maximum force acting on the bar is Fmax and maximum stress produced in the bar is σmax.

Write the expression of minimum stress acting on the bar.

σmin=FminA (XXVII)

Here, the minimum force acting on the bar is Fmin and minimum stress acting on the bar is σmin.

Write the expression of nominal amplitude stress.

σao=|σmaxσmin2| (XXVIII)

Here the nominal amplitude stress is σao.

Write the expression of nominal midrange stress.

σmo=|σmax+σmin2| (XXIX)

Here, the nominal amplitude stress for is σmo.

Write the expression of amplitude component.

σa=Kf×σao (XXX)

Here, the amplitude component is σa and the above expression is valid when notch present in the component.

Write the expression of midrange component.

σm=Kf×σmo . (XXXI)

Here, the midrange component is σm and the above expression is valid when notch present in the component.

Write the Expression of yield factor of safety.

ny=|Syσmin| (XXXII)

Here the yield factor of safety is ny and the yield strength is Sy.

Write the expression of fatigue factor of safety using the modified Goodman criterion.

(nf)G=Seσa (XXXIII)

Here the fatigue factor of safety is nf.

Write the expression of number of cycle in case of completely reversed stress.

N=(σreva)1/b

Here, the number of cycle are N, completely reversed stress is σrev, constants are a and b.

Simplify the Equation (IX) for completely reversed stress and substitute σ'a for σrev in above Equation.

N=(σaa)1/b (XXXIV)

Write the expression of constant a.

a=(fSut)2Se (XXXV)

Here, the strength fraction is f.

Write the expression of the constant b.

b=13log(fSutSe) (XXXVI)

Conclusion:

Substitute 12kN for Fmax and 190mm2 for A in Equation (XXVI).

σmax=12kN190mm2=0.0632(kN/mm2)(1000N1kN)=0.0632(kN/mm2)(1000N1kN)(1MPa1N/mm2)=63.2MPa

Substitute 28kN for Fmin and 190mm2 for A in Equation (XXVII).

σmin=28kN190mm2=0.14737(kN/mm2)(1000N1kN)=0.14737(kN/mm2)(1000N1kN)(1MPa1N/mm2)=147.4MPa

Substitute 63.2MPa for σmax and 147.4MPa for σmin in Equation (XXVIII).

σao=|(63.2MPa)(147.4MPa)2|=210.6MPa2=105.3MPa

Substitute 63.2MPa for σmax and 147.4MPa for σmin in Equation (XXIX).

σmo=|(63.2MPa)+(147.4MPa)2|=84.2MPa2=42.1MPa

Substitute 105.2MPa for σao and 2.20 for Kf in Equation (XXX).

σa=2.20×105.2MPa=231.44MPa231.4MPa

Substitute 42.1MPa for σmo and 2.20 for Kf in Equation (XXXI).

σm=2.20×(42.1MPa)=92.63MPa=92.62MPa

Substitute 490MPa for Sy and 147.4MPa for σmin in Equation (XXXII).

ny=|490MPa147.4MPa|=490147.4=3.32

Thus, the yield factor of safety is 3.32.

Substitute 208.6MPa for Se, 231.4MPa for σa in Equation (XXXIII).

(nf)G=208.6MPa231.4MPa=208.6231.4=0.905

Thus, the fatigue factor of safety is 0.905.

From fig-618 “Fatigue strength fraction f of Sut at 103 cycles for Se and S'e at 106 cycles” the value of f is 0.87.

Substitute 0.87 for f, 590MPa and 208.6MPa for Se in Equation (XXXV).

a=((0.87)(590MPa))2208.6MPa=263476.89208.6MPa=1263.07MPa1263MPa

Substitute 0.87 for f, 590MPa for Sut and 208.6MPa for Se in Equation (XXXVI).

b=13log((0.87)(590MPa)208.6MPa)=13(0.39105)=0.130350.1304

Substitute 1263MPa for a, 0.1304 for b, and 231.4MPa for σa in Equation (XIV).

N=(231.4MPa1263Mpa)1/(0.1304)=(0.1832)1/(0.1304)=448897.52cycles446000cycles

Thus, the number of cycle to failure is 446000cycles.

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Chapter 6 Solutions

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

Ch. 6 - Two steels are being considered for manufacture of...Ch. 6 - A 1-in-diamctcr solid round bar has a groove...Ch. 6 - A solid square rod is cantilevered at one end. The...Ch. 6 - A rectangular bar is cut from an AISI 1020...Ch. 6 - A solid round bar with diameter of 2 in has a...Ch. 6 - The rotating shaft shown in the figure is machined...Ch. 6 - The shaft shown in the figure is machined from...Ch. 6 - Solve Prob. 6-17 except with forces F1 = 1200 lbf...Ch. 6 - Bearing reactions R1 and R2 are exerted on the...Ch. 6 - A bar of steel has the minimum properties Se = 40...Ch. 6 - Repeat Prob. 6-20 but with a steady torsional...Ch. 6 - Repeat Prob. 6-20 but with a steady torsional...Ch. 6 - Repeat Prob. 6-20 but with an alternating...Ch. 6 - A bar of steel has the minimum properties Se = 40...Ch. 6 - The cold-drawn AISI KUO steel bar shown in the...Ch. 6 - Repeat Prob. 6-25 for a load that fluctuates from...Ch. 6 - An M14 2 hex-head bolt with a nut is used to...Ch. 6 - The figure shows a formed round-wire cantilever...Ch. 6 - The figure is a drawing of a 4- by 20-mm latching...Ch. 6 - The figure shows the free-body diagram of a...Ch. 6 - Solve Prob. 6-30 except let w1 = 2.5 in. w2 = l.5...Ch. 6 - For the part in Prob. 630, recommend a fillet...Ch. 6 - Prob. 33PCh. 6 - Prob. 34PCh. 6 - A part is loaded with a combination of bending,...Ch. 6 - Repeat the requirements of Prob. 6-35 with the...Ch. 6 - 6-37 to 6-46For the problem specified in the build...Ch. 6 - 6-37 to 6-46For the problem specified in the build...Ch. 6 - 637 to 646 For the problem specified in the table,...Ch. 6 - For the problem specified in the table, build upon...Ch. 6 - 6-37 to 6-46 For the problem specified in the...Ch. 6 - 6-37 to 6-46 For the problem specified in the...Ch. 6 - 6-37 to 6-46 For the problem specified in the...Ch. 6 - Problem Number Original Problem, Page Number 637...Ch. 6 - 6-37 to 6-46 For the problem specified in the...Ch. 6 - 6-37 to 6-46 For the problem specified in the...Ch. 6 - 6-47 to 6-50 For the problem specified in the...Ch. 6 - 6-47 to 6-50 For the problem specified in the...Ch. 6 - Prob. 49PCh. 6 - Prob. 50PCh. 6 - 6-51 to 6-53 For the problem specified in the...Ch. 6 - 6-51 to 6-53 For the problem specified in the...Ch. 6 - 6-51 to 6-53 For the problem specified in the...Ch. 6 - Solve Prob. 6-17 except include a steady torque of...Ch. 6 - Solve Prob. 618 except include a steady torque of...Ch. 6 - In the figure shown, shaft A, made of AISI 1020...Ch. 6 - A schematic of a clutch-testing machine is shown....Ch. 6 - For the clutch of Prob. 657, the external load P...Ch. 6 - A flat leaf spring has fluctuating stress of max =...Ch. 6 - A rotating-beam specimen with an endurance limit...Ch. 6 - A machine part will be cycled at 350 MPa for 5...Ch. 6 - The material properties of a machine part are Sut...Ch. 6 - Repeat Prob. 662 using the Goodman criterion....
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