The aerodynamics of helicopter flight is analyzed for hover, translating, and partial power flight. Theory and experimental results are used to predict aircraft performance. The course analyzes the dynamic response of the rotor system and the performance aspects of the vehicle as a whole. This is followed by a design workshop, during which cadets complete the initial sizing of a helicopter to meet specific mission requirements. The course includes one flight lab in a helicopter, a laboratory examining rotor power and thrust utilizing a whirl stand apparatus, and one field trip to a commercial helicopter company.
Lessons
28 @ 75 min (2.000 Att/wk)
Labs
2 @ 120 min
Special requirements
Either AE201 or ME202 are required as a pre-requisite but may be waived with validation exercise on structured programming and AE Program Director approval.
