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What is Supersonic Thin Airfoil Theory Analysis about?

1. The governing equation for potential flow over a thin airfoil in supersonic flow is hyperbolic. Its characteristics are straight lines with slopes of ±1/β, where β is the Mach angle. 2. The general solution of the governing equation is the sum of two functions, where each function depends on only one characteristic parameter. 3. In supersonic flow, information cannot travel upstream of the characteristics emanating from the airfoil

Author

Mohamed Askar

Language

EN