Jun 25, 2022  
2015-2016 Undergraduate Catalog 
    
2015-2016 Undergraduate Catalog [ARCHIVED CATALOG]

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AES 4610 - Aerodynamic Design



Credits: 3

Prerequisite(s): AES 3530, or permission of instructor

Description: Students analyze aerodynamics in both the subsonic and supersonic range. Airfoil theory, the calculations of lift and drag, National Advisory Committee for Aeronautics (NACA) derived airfoils, and their applications will be studied. A wind tunnel laboratory is utilized to conduct experimentation with the Bernoulli equation and Reynolds number and to test aerodynamic properties of various structures.



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