Physical analysis of compressibility effects in the transonic flow around a supercritical airfoil at high Reynolds number by numerical simulation

【Author】

Damien Szubert;Fernando Grossi;Marianna Braza;Yannick Hoarau;Gilles Harran;Alain Sevrain;

【Abstract】

<正>In transonic flow,specific combinations of the Mach number and of the angle of attack may engender a large-amplitude periodic motion of the shock-wave around a wing.This is triggered by the wake's large scale instability and leads to a complex shockwave /boundary layer interaction.This phenomenon can create

【Keywords】

flow;Physical analysis of compressibility effects in the transonic flow around a supercritical airfoil at high Reynolds number by numerical simulation;high;

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