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clc
//
//Variable declaration
D=60 // Width(mm)
d=40 // Width(mm)
r=8 // Radius(mm)
K=1.82 // Stress-concentration factor
Smax=165 // Allowable normal stress(MPa)
//Calculation
eave=(165/1.82) // Average stress in the narrower portion(MPa)
P=((40*10*eave)/(1000)) // Largest Axial Load(kN)
// Results
printf("\n Largest Axial Load =%1f in' ,P)
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