MAE 3253

Applied Aerodynamics and Performance

Oklahoma State University · UGRD · Fall 2026

1 section
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Description: Relevant fluid properties; standard atmospheres; mathematical models of flows about bodies. Characteristic parameters of airfoils and wings. Thin airfoil theory and flows about finite wings. Boundary layers. Propeller theory. Supersonic and hypersonic flows about wings and lifting bodies. Drag polars. Power required for level flight. Rate of climb and descent. Steady turns. Maximum range and endurance. Design applications.

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Class #oklahoma_state-5426Fall 2026UGRD
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