For example, let’s examine the pitching moment imposed on a wing cross-section, caused by an aileron deflection movement downward. Assume the centroid is at the midpoint of the wing chord (not including the aileron). Using the examples provided in the presentation slides, what will be the pitching moments for the following upward forces: 20 lbs., 30 lbs., 40 lbs., and 50 lbs.? Can you now see why a wing needs a certain amount of rigidity? Please explain.
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Physics, 22.06.2019 18:00
By what primary heat transfer mechanism does the sun warm the earth?
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Physics, 22.06.2019 18:00
Atank is filled with an ideal gas at 400 k and pressure of 1.00 atm . part a the tank is heated until the pressure of the gas in the tank doubles. what is the temperature of the gas?
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Physics, 22.06.2019 23:20
Consider a production line with five stations. station 1 can produce a unit in 9 minutes. station 2 can produce a unit in 10 minutes. station 3 has two identical machines, each of which can process a unit in 12 minutes (each unit only needs to be processed on one of the two machines. station 4 can produce a unit in 5 minutes. station 5 can produce a unit in 8 minutes. which station is the bottleneck station?
Answers: 2
Physics, 23.06.2019 00:00
You can melt ice by applying pressure because the solid/liquid line has a slope.
Answers: 3
For example, let’s examine the pitching moment imposed on a wing cross-section, caused by an aileron...
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