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AESP 265 - Aerodynamics I Incompressible FlowCredits: 3Fundamentals 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. Prerequisites: MATH 242, EMCH 201 |
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