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MECH 537 High-Speed Aerodynamics (3 unit茅s)

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Offered by: G茅nie m茅canique (G茅nie et l'architecture)

Vue d'ensemble

G茅nie m茅canique : Equations of compressible flows. Planar and conical shock waves. Expansion and shock wave interference; shock tubes. Method of characteristics. Supersonic nozzle design. Aerofoil theory in high subsonic, supersonic and hypersonic flows. Conical flows. Yawed, delta and polygonal wings; rolling and pitching rotations. Wing-body systems. Elements of transonic flows.

Terms: This course is not scheduled for the 2021-2022 academic year.

Instructors: There are no professors associated with this course for the 2021-2022 academic year.

  • (3-0-6)

  • Pre/Corequisite (Undergraduate): MECH 533

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