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Apr 20, 2024
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AE 3710 - Aerodynamics II
An introduction to compressible aerodynamics and boundary layer theory, including subsonic and supersonic flows over wings and bodies and viscous flows. Emphasis is placed on application of the basic theory for solving practical aerodynamic problems in the design of flight vehicles.
Prerequisites & Corequisites: Prerequisites: AE 3610; MATH 3740; ME 2580.
Credits: 3 hours
Restrictions: This course restricted to majors in aerospace engineering.
When Offered: Spring
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