U. S. Centennial of Flight - History of Flight

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Images from: Theories of Flight (Aerodynamics)

	Total aircraft shocks at Mach 1 Credit - NASA
	Shock waves with different swept wings Credit - NASA
	Delta-wing plane Credit - NASA
	Wing drag coefficient vs Mach number Credit - NASA
	Lift-to-drag ratio vs Mach number for different wings Credit - NASA
	Wing sweep on different planes Credit - NASA
	Canards and double delta wings Credit - NASA
	Vortices on lift vs angle of attack Credit - NASA
	Supersonic aircraft Credit - NASA
	U.S. SST configurations Credit - NASA
	Advanced SST configuration Credit - NASA
	Sonic boom generation Credit - NASA
	Overpressure vs various supersonic parameters Credit - NASA
$Refraction of shock waves$	Refraction of shock waves Credit - NASA