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 2020

Instructors: Jovan Nedic (Winter)