Texas A&M University 3 credits AERO
Conservation of mass and momentum; Reynolds transport theorem; fundamentals of incompressible flow, rotationality, potential flow, superposition, circulation, lift, thin airfoil theory, elliptic wing theory and induced drag. Prerequisite: Grade of C or better in AERO 201, AERO 212; grade of C or better in AERO 222 and MATH 308, or concurrent enrollment.
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