1010611
9781563475771
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.Yechout, Thomas R. is the author of 'Introduction to Aircraft Flight Mechanics Performance, Static Stability, Dynamic Stability, and Classical Feedback Control' with ISBN 9781563475771 and ISBN 1563475774.
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