Disturbance evolution in a Mach 4.8 boundary layer with separation

【Author】

Olaf Marxen;Thierry Magin;Gianluca laccarino;

【Abstract】

<正>Predicting the location of laminar-turbulent transition on the surface of supersonic or hypersonic vehicles is important for the design of thermal protection systems.Knowledge of the mechanisms leading to transition is required to improve transition pre-

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