MECH 532 — Aircraft Performance, Stability and Control

Name: MECH 532 — Aircraft Performance, Stability and Control
Rating: 3.02 (96 reviews)

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.

Rating: 3.02 out of 5 from 96 student reviews
Difficulty: 4.40 out of 5
Credits: 3
Faculty: Faculty of Engineering
Department: Mechanical Engineering
Prerequisite (Graduate): MECH 533