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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 2016-2017 academic year.
Instructors: There are no professors associated with this course for the 2016-2017 academic year.
(3-0-6)
Pre/Corequisite (Undergraduate): MECH 533