Answer:
The smallest radius at the junction between the cross section that can be used to transmit the torque is 0.167 inches.
Explanation:
Torsional shear stress is determined by the following expression:

Where:
- Torque, measured in
.
- Radius of the cross section, measured in inches.
- Torsion module, measured in quartic inches.
- Torsional shear stress, measured in pounds per square inch.
The radius of the cross section and torsion module are, respectively:


Where
is the diameter of the cross section, measured in inches.
Then, the shear stress formula is now expanded and simplified as a function of the cross section diameter:


In addition, diameter is cleared:

![D = 2\cdot \sqrt[3] {\frac {2\cdot T}{\pi\cdot \tau}}](https://tex.z-dn.net/?f=D%20%3D%202%5Ccdot%20%5Csqrt%5B3%5D%20%7B%5Cfrac%20%7B2%5Ccdot%20T%7D%7B%5Cpi%5Ccdot%20%5Ctau%7D%7D)
If
and
, then:
![D = \sqrt[3]{\frac{2\cdot (710\,lbf\cdot in)}{\pi \cdot (12000\,psi)} }](https://tex.z-dn.net/?f=D%20%3D%20%5Csqrt%5B3%5D%7B%5Cfrac%7B2%5Ccdot%20%28710%5C%2Clbf%5Ccdot%20in%29%7D%7B%5Cpi%20%5Ccdot%20%2812000%5C%2Cpsi%29%7D%20%7D)


The smallest radius at the junction between the cross section that can be used to transmit the torque is 0.167 inches.
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Answer:
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Answer:
0.21
Explanation:
This would have been a fairly easy one, except for that the first part of the question is missing, and as such, I'd assume a value.
We need to use chord, so, I'm assuming the length of the chord to be 0.045 m
The Area is given by the formula
Area = span * chord
Area = 0.245 * 0.045
Area = 0.011 m²
This area gotten, is what we then divide the glider weight by to get our answer.
Lee = area / weight
Lee = 0.011 / 0.0523
Lee = 0.21
Therefore, using the values of the chord I'd assumed, the Lee of the same wing is 0.21