Concave Bump for Impinging-Shock Control in Supersonic Flows

In the present study, a novel concave bump for impinging-shock control in two-dimensional supersonic flows is investigated. An analytical method for preliminary bump design based on a generalized shape of a shock-canceling bump has been developed and verified numerically. An extensive proof-of-conce...

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Veröffentlicht in:	AIAA journal 2022-05, Vol.60 (5), p.2749-2766
Hauptverfasser:	Schülein, Erich, Schnepf, Christian, Weiss, Sebastian
Format:	Artikel
Sprache:	eng
Schlagworte:	Deflection High speed Impingement Mach number Optimization Pressure loss Pressure recovery Reduction Reynolds number Separation Supersonic flow Two dimensional analysis Two dimensional flow
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