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Overview
Mechanical Engineering : Aircraft performance criteria such as range, endurance, rate of climb, maximum ceiling for steady and accelerated flight. Landing and take-off distances. Static and dynamic stability in the longitudinal (stick-fixed and stick-free) and coupled lateral and directional modes. Control response for all three modes.
Terms: Winter 2011
Instructors: Nahon, Meyer (Winter)
- (3-0-6)
- Prerequisite (Undergraduate): (MECH 412 or MECH 419), MECH 533
- Prerequisite (Graduate): MECH 533