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Introduce a Girl to Engineering Day
Girls, please solve this problem!
(And if you get the answer, please tell me the answer because I don't want to do it.)
Assume that the pitching moment characteristics of a propeller driven airplane are as shown in the figure below. If the elevator deflection will generate an incremental pitching moment coefficient given by: ∆Cm = Cm(δe), calculate and plot the elevator angle, δe, to trim versus the thrust coefficient for zero flaps and for flaps down. Assume that Cm(δe) = -0.02 1/deg and α = 6 deg.
National Chili Day
I'm having chili for dinner. I suggest you do the same.