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22-Mec-B1 Advanced Machine Design · May 2017

Question 4 of 6: Notched bar — axial fatigue

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Exams — 16-Mec-B1 Advanced Machine Design, May 2017. Open-book, 3 hours, 100 marks. Part I (Problems 1–2) is compulsory; only three of the four Part II problems (Problems 3–6) are required. All six problems are solved as a study resource. “State all assumptions clearly… assume any missing data and properly state it” is an explicit exam instruction, invoked in Problem 2.

Reference texts. R.G. Budynas & J.K. Nisbett, Shigley’s Mechanical Engineering Design, 10th ed. (shafts & deflection §7 & §4, fasteners §8, clutches/brakes §16, journal bearings §12, power screws §8-2); R.C. Juvinall & K.M. Marshek, Fundamentals of Machine Component Design (brakes, bearings, screws); R.C. Hibbeler, Mechanics of Materials (beam deflection, impact); R.L. Norton, Machine Design (fatigue, stress concentration).

Question 4: Notched bar — axial fatigue (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Rectangular bar $b=22$ mm (thickness) × $w=30$ mm (width), transverse central hole $d=10$ mm through the 30-mm face. Axial load cycles $F_{min}=-4$ kN to $F_{max}=12$ kN. Machined, room temperature, $S_{ut}=500$ MPa, reliability 99.999%.

Given data
QuantitySymbolValue
Width across hole$w$30 mm
Thickness$b$22 mm
Hole diameter$d$10 mm
Min / max load$F_{min}$ / $F_{max}$−4 kN / 12 kN
Ultimate strength$S_{ut}$500 MPa
Reliability$R$99.999%

Find. (1) fatigue stress-concentration factor $K_f$; (2) worst mean and alternating stresses; (3) infinite-life fatigue factor of safety.

Approach. Read the geometric factor $K_t$ for a transverse hole (net-section basis) at $d/w=1/3$, apply notch sensitivity to get $K_f$; compute mean and alternating loads, divide by the net area and scale by $K_f$; build the corrected endurance limit with the Marin factors for axial loading and 99.999% reliability, then apply the Goodman line.

  1. Stress-concentration factor. For a flat bar with a transverse central hole in axial tension, at $d/w=10/30=0.333$, the net-section chart gives $K_t\approx2.35$. Notch sensitivity from the Neuber constant for steel ($\sqrt{a}=0.062$ in$^{1/2}$ at $S_{ut}=500$ MPa, hole radius $r=5$ mm) is $$q=\frac{1}{1+\sqrt{a}/\sqrt{r}}=0.83,\qquad K_f=1+q(K_t-1)=\boxed{2.12}.$$
  2. Mean and alternating loads. $$F_m=\tfrac12(F_{max}+F_{min})=4\text{ kN},\qquad F_a=\tfrac12(F_{max}-F_{min})=8\text{ kN}.$$
  3. Net area & nominal stresses. The hole removes material on the loaded section: $A_{net}=(w-d)\,b=(30-10)(22)=440\ \text{mm}^2$. Nominal $\sigma_{m0}=F_m/A_{net}=9.09$ MPa, $\sigma_{a0}=F_a/A_{net}=18.18$ MPa.
  4. Worst-case (notch-peak) stresses. Applying $K_f$ to both components, $$\boxed{\sigma_m=K_f\sigma_{m0}=19.3\text{ MPa},\qquad \sigma_a=K_f\sigma_{a0}=38.5\text{ MPa}.}$$
  5. Corrected endurance limit. $S_e'=0.5S_{ut}=250$ MPa. Marin factors: surface $k_a=4.51\,S_{ut}^{-0.265}=0.869$ (machined); size $k_b=1$ (axial — no size effect); load $k_c=0.85$ (axial); temperature $k_d=1$; reliability $k_e=0.659$ (99.999%). Hence $$S_e=k_a k_b k_c k_d k_e\,S_e'=0.869(1)(0.85)(1)(0.659)(250)=\boxed{121.6\text{ MPa}}.$$
  6. Infinite-life factor of safety (Goodman). $$\frac{1}{n_f}=\frac{\sigma_a}{S_e}+\frac{\sigma_m}{S_{ut}}=\frac{38.5}{121.6}+\frac{19.3}{500}=0.317+0.039,$$ $$\boxed{n_f=2.82}.$$ The factor exceeds unity by a wide margin, so the notched bar has infinite life with a comfortable reserve.
Problem 4 — results
QuantityValue
Stress-concentration factor $K_t$ / $K_f$2.35 / 2.12
Mean / alternating load4 kN / 8 kN
Net area440 mm²
Worst $\sigma_m$ / $\sigma_a$19.3 MPa / 38.5 MPa
Corrected endurance limit $S_e$121.6 MPa
Fatigue safety factor (infinite life)2.82