Tag: Aerospace Engineering
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Draw a diagram that explains the change in angle of attack on the canard on the canard due to a pitch rate, q. Show how CMq will change. Make sure to include a drawing of the CG, freestream, pitch rate direction, the induced flow on the canard, the induced angles on the canard and the resulting forces and moments.
Aerospace Engineering 1) Show, by a drawling below, how a v velocity on the following airplane can become a u . What angular rate would need to be present (indicate variable and sign)? Show 2 frames of the motion. 2) Show, by a drawling below, how a w velocity on the following airplane can become…