Question 5.5: Consider the wrench in Ex. 5–3, Fig. 5–16, as made of cast i...

Consider the wrench in Ex. 5–3, Fig. 5–16, as made of cast iron, machined to dimension. The force F required to fracture this part can be regarded as the strength of the component part. If the material is ASTM grade 30 cast iron, find the force F with
(a) Coulomb-Mohr failure model.
(b) Modified Mohr failure model.

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We assume that the lever DC is strong enough, and not part of the problem. Since grade 30 cast iron is a brittle material and cast iron, the stress-concentration factors K_{t}  and  K_{ts} are set to unity. From Table A–24, the tensile ultimate strength is 31 kpsi and the compressive ultimate strength is 109 kpsi. The stress element at A on the top surface will be subjected to a tensile bending stress and a torsional stress. This location, on the 1-indiameter section fillet, is the weakest location, and it governs the strength of the assembly. The normal stress σ_{x} and the shear stress at A are given by

Table A–24  Mechanical Properties of Three Non-Steel Metals (a) Typical Properties of Gray Cast Iron [The American Society for Testing and Materials (ASTM) numbering system for gray cast iron is such that the numbers correspond to the minimum tensile strength in kpsi. Thus an ASTM No. 20 cast iron has a minimum tensile strength of 20 kpsi. Note particularly that the tabulations are typical of several heats.]

 

Fatigue Stress- Concentration Factor Brinell Hardness Endurance Limit* , kpsi Modulus of Elasticity, Mpsi Shear Modulus of Rupture Compressive Strength , kpsi Tensile Strength S_{ut} kpsi ASTM Number
Torsion Tension†
1.00 156 10 3.9–5.6 9.6–14 26 83 22 20
1.05 174 11.5 4.6–6.0 11.5–14.8 32 97 26 25
1.10 201 14 5.2–6.6 13–16.4 40 109 31 30
1.15 212 16 5.8–6.9 14.5–17.2 48.5 124 36.5 35
1.25 235 18.5 6.4–7.8 16–20 57 140 42.5 40
1.35 262 21.5 7.2–8.0 18.8–22.8 73 164 52.5 50
1.50 302 24.5 7.8–8.5 20.4–23.5 88.5 187.5 62.5 60

*Polished or machined specimens.
†The modulus of elasticity of cast iron in compression corresponds closely to the upper value in the range given for tension and is a more constant value than that for tension.

σ_{x} =K_{t} \frac {M}{I/c} = K_{t} \frac {32M}{πd^{3}} = (1) \frac {32(14F)}{π(1)^{3}} = 142.6F
τ_{xy} = K_{ts} \frac {Tr}{J} = K_{ts} \frac {16T}{πd^{3}} = (1) \frac {16(15F)}{π(1)^{3}} = 76.4F

From Eq. (3–13) the nonzero principal stresses σ_{A} and σ_{B} are

σ_{1}, σ_{2} =\frac {σ_{x} + σ_{y}}{2}± \sqrt { \left(\frac {σ_{x} – σ_{y}}{2} \right)+τ^{2}_{xy}}                   (3-13)

σ_{A}, σ_{B} =\frac {142.6F+ 0}{2}± \sqrt { \left(\frac {142.6F- 0}{2} \right)+(76.4F)^{2}} = 175.8F,−33.2F

This puts us in the fourth-quadrant of the σ_{A} , σ_{B} plane.
(a) For BCM, Eq. (5–31b) applies with n = 1 for failure.

\frac {σ_{A}}{S_{ut}} −\frac {σ_{B}}{S_{uc}} =\frac {1}{n}              σ_{A} ≥ 0 ≥ σ_{B}                         (5–31b)

\frac {σ_{A}}{S_{ut}} −\frac {σ_{B}}{S_{uc}}=\frac {175.8F}{31(10^{3})} − \frac {(−33.2F)}{109(10^{3})} = 1

Solving for F yields

F = 167 lbf

(b) For MM, the slope of the load line is |σ_{B}/σ_{A}| = 33.2/175.8 = 0.189 <1.
Obviously, Eq. (5–32a) applies.

σ_{A} ≥ 0 ≥ σ_{B}   and  | \frac {σ_{B}}{σ_{A}} | ≤ 1             (5–32a)

\frac {σ_{A}}{S_{ut}}=\frac {175.8F}{31(10^{3})}=1

F = 176 lbf

As one would expect frominspection of Fig. 5–19, Coulomb-Mohr ismore conservative.

 

 

5.19

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