Fundamentals of AerodynamicsIn keeping with the successful previous edition, Anderson carries over the second edition content into the third edition while adding selected topics and examples. New coverage on the Computational Fluid Dynamics (CFD) and new illustrations to help the students to understand the basic conepts. More than a dozen "design boxes" are included to help students focus on the practical applications. |
Common terms and phrases
adiabatic aerodynamic airfoil section airplane angle of attack aspect ratio Bernoulli's equation body boundary layer C₁ calculate camber Chapter compressible Consider constant control volume Couette flow curve delta wing denoted direction downstream drag coefficient example finite wing flat plate flight flow field fluid element freestream given by Equation heat Hence hypersonic incompressible flow increases induced drag integral inviscid flow isentropic laminar leading edge lift coefficient lift slope M₁ Mach number momentum NACA normal shock wave Note nozzle oblique shock obtained p₁ panel Prandtl pressure coefficient pressure distribution Reynolds number shear stress shock wave shown in Figure sketched in Figure solution stagnation point streamline subsonic Substituting Equation supersonic flow surface temperature thin airfoil three-dimensional total pressure trailing edge two-dimensional vector velocity viscous flow vortex sheet vortices wall wind tunnel zero ди др дх ду