Introduction to high speed aerodynamics, high speed A/C components andlayout. Supersonic flows around airfoils, shock waves, Normal shock waves, Obliqueshock waves, Prandtl Meyer shock expansion, linear theory, Busman’s theory. Finitewings in supersonic flow, conical method, singularity distribution method, application on lifting surface. Sharp nosed body of revolution. Wing body interference, wing tailinterference. Drag components
