An interferential streak instability of hypersonic boundary layer over a circular cone

【Author】

Qing Shen;Feng Ji;Xiangjiang Yuan;Qiang Wang;

【Abstract】

<正>A study on the stability of hypersonic boundary layer over a 5μm;half-angle cone with 1 mm nose radius has been performed at 0.5 and ordm;angle of attack(AoA) with Mach number 6.0 and unit Reynolds number 1.0×10~7/m.After obtaining the undisturbed steady flow using NND finite scheme,the stability characteristic at different region on the windward and leeward meridian

【Keywords】

show;An interferential streak instability of hypersonic boundary layer over a circular cone;

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