AESP 265

Aerodynamics I Incompressible Flow

University of South Carolina-Columbia · UGRD · Fall 2026

1 section

Catalog description

Fundamentals of inviscid, incompressible flow. Derivation of basic equations for lift, drag and aerodynamic moments through dimensional analysis. Two dimensional flow over airfoils. Airfoil characteristics. Thin airfoil theory, finite wing theory. Wing and body interactions. Aerodynamic drag characteristics. Boundary layers.

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Class #south_carolina_columbia-AESP265Fall 2026UGRD3 credits

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