- Joined
- Nov 23, 2014
- Messages
- 2,609
Oops, told you it'd been a long time since I'd had the class. I am wrong on the formula:
tau = (T x L) / (J x G) is not torsional stress, it's the angle of rotation.
The stress formula is:
tau (reference I found online uses theta for the angle, I was taught tau) = Tmax / J
The comparison I mentioned above is still correct; polar moment of inertia is still in the denominator. I guess my memory from a class in college 43 years ago is lacking!
Bruce
tau = (T x L) / (J x G) is not torsional stress, it's the angle of rotation.
The stress formula is:
tau (reference I found online uses theta for the angle, I was taught tau) = Tmax / J
The comparison I mentioned above is still correct; polar moment of inertia is still in the denominator. I guess my memory from a class in college 43 years ago is lacking!
Bruce