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MECH 531 Aeroelasticity (3 credits)

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Offered by: Mechanical Engineering (Faculty of Engineering)

Overview

Mechanical Engineering : Wing divergence using strip-theory aerodynamics. Effect of aircraft flexibility on the control and stability. Flutter calculations for two-dimensional wings with discussion of three-dimensional effects. Some examples of aeroelastic instability, and the relevant analysis of non-aeronautical problems.

Terms: This course is not scheduled for the 2010-2011 academic year.

Instructors: There are no professors associated with this course for the 2010-2011 academic year.

  • (3-0-6)
  • Prerequisite (Undergraduate): MECH 419 or MECH 315 and MECH 533
  • Prerequisite (Graduate): MECH 533
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