ON SLENDER AIRFOIL THEORY FOR NON-EQUILIBRIUM FLOW

An exact theory for non-equilibrium flow past a thin airfoil is given. Green's function technique is used to solve the boundary value problem for the governing third order equation. Upon satisfying the boundary condition on the airfoil surface an integral equation is obtained which has an exact...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	Ryhming,Inge L
Format:	Report
Sprache:	eng
Schlagworte:	AIRFOILS BOUNDARY LAYER GAS FLOW GREENS FUNCTIONS INTEGRAL EQUATIONS MATHEMATICAL ANALYSIS PARTIAL DIFFERENTIAL EQUATIONS SUPERSONIC FLOW
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