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Machine Design

Machine Design
The endurance limit in shear of carbon steel can be obtained by multiplying the endurance limit in flexure by a factor of

0.65
0.45
0.75
0.55

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Machine Design
The static tooth load should be __________ the dynamic load.

Less than
None of these
Greater than
Equal to

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Machine Design
Aircraft body is usually fabricated by

Pre-casting
Casting
Welding
Riveting

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Machine Design
Lewis form factor for 14½° composite and full depth involute system is (where T = Number of teeth)

0.124 - (0.684/T)
None of these
0.175 - (0.841/T)
0.154 - (0.912/T)

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Machine Design
The connecting rod bolts are tightened up so that tightening stress

Is 50% of yield point
Is just sufficient to hold parts together
Approaches yield point
Is about yield point divided by safety factor

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Machine Design
The yield point in static loading is __________ as compared to fatigue loading.

Same
Higher
None of these
Lower

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