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MECH 5101 [0.5 credit] (MCG 5311) Dynamics and Aerodynamics of Flight

Static stability theory. Euler's equations for rigid body motion; the linearized equations of motion; stability derivatives and their estimation. Longitudinal and lateral dynamic response of an aircraft to control and disturbance.
Includes: Experiential Learning Activity
Also listed as MAAJ 5151.
Also offered at the undergraduate level, with different requirements, as AERO 4308, for which additional credit is precluded.