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MECH 532 Aircraft Performance, Stability and Control (3 credits)

Offered by: Mechanical Engineering (Faculty of Engineering)

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 2013

Instructors: There are no professors associated with this course for the 2012-2013 academic year.

  • (3-0-6)
  • Prerequisite (Undergraduate): (MECH 412 or MECH 419), MECH 533
  • Prerequisite (Graduate): MECH 533