Section 12: 普朗特经典升力线理论(3 学时)
Section 13: 可压缩流动控制方程;激波(3 学时)
Section 14: 正激波特性的计算(3 学时)
Section 15: 斜激波(3 学时)
Section 16: 膨胀波(3 学时)
Section 1: Some fundamental aerodynamic variables; Aerodynamic force and moment; Center of pressure; Dimensional
analysis and flow similarity(3 credit hours)
Section 2: Types of flow; Continuity equation; Momentum equation; Energy equation(3 credit hours)
Section 3: Stream function; Velocity potential; Bernoulli’s equation(3 credit hours)
Section 4: Laplace’s equation; Uniform flow; Source flow(3 credit hours)
Section 5: Doublet flow; Flow over a circular cylinder(3 credit hours)
Section 6: The Kutta-Joukowski theorem and the generation of lift(3 credit hours)
Section 7: Nomenclature and characteristics of airfoil; The vortex sheet(3 credit hours)
Section 8: The Kutta condition(3 credit hours)
Section 9: Classical thin airfoil theory: the symmetric airfoil and cambered airfoil(3 credit hours)
Section 10: The vortex panel numerical method(3 credit hours)
Section 11: Downwash and induced drag; The vortex filament, the Biot-Savart law and Helmholtz’s theorems(3 credit
hours)
Section 12: Prandtl’s classical lifting-line theory(3 credit hours)
Section 13: Governing equations of compressible flow; Shock waves(3 credit hours)
Section 14: Calculation of normal shock-wave properties(3 credit hours)
Section 15: Oblique shock waves(3 credit hours)
Section 16: Expansion waves(3 credit hours)