Fundamentals of Aerodynamics
John D. Anderson Jr.
The definitive text on aerodynamics. Master thin airfoil theory, finite wings, and compressible flow through interactive analysis tools.
The definitive text on aerodynamics. Master thin airfoil theory, finite wings, and compressible flow through interactive analysis tools.
Potential flow, circulation, and the foundations of lift. Kutta-Joukowski theorem in action before viscosity enters the picture.
When flow turns through a compression corner an oblique shock forms. Through an expansion corner a centered expansion fan (Prandtl-Meyer) smoothly accelerates and turns the flow.
The thin viscous layer that makes or breaks aircraft and rockets. Laminar vs turbulent, separation, and skin friction drag.
Thin airfoil theory gives the foundation for Cl(α) and the Kutta condition. Prandtl's lifting-line theory shows how finite aspect ratio creates induced drag and reduces effective angle of attack.
The single most useful plot in aerodynamics: C_D vs C_L. How to read L/D max and its direct impact on range and glide.
Newtonian theory, high-temperature effects, and the extreme environment faced by reentry vehicles and boost-glide weapons.
When the boundary layer and shock layer talk to each other at Mach 10+.
Putting it together: ascent loads, base drag, staging aerodynamics, and booster return (Falcon 9, Starship).