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Course
Description
Rotor
aerodynamics: blade element theory, momentum theory, Goldstein's
theory, modem vortex theories. Comparison of theory and experiment
in hover, transition and high speed flight, rotor blade motion:
articulated and hingeless Rotors. Helicopter performance estimation
in level flight, autorotation and climb; control required
to trim in steady flight.
Prerequisites
3
lecture hours
3 semester hours
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