AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER 被引量：1

AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER

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摘要 Detailed distributions of heat flux in the region of shock wave and turbulent boundary layer interaction induced by a cylinder were measured in the shock tunnel Oil flow patterns and Schlieren photo- graphs were taken.Empirical relations were given for determining separation shock angle,peaks of heat flux and their locations on both cylinder leading edge and flat plate surface,and other characteristic parameters of the interaction region. Detailed distributions of heat flux in the region of shock wave and turbulent boundary layer interaction induced by a cylinder were measured in the shock tunnel Oil flow patterns and Schlieren photo- graphs were taken.Empirical relations were given for determining separation shock angle,peaks of heat flux and their locations on both cylinder leading edge and flat plate surface,and other characteristic parameters of the interaction region.

作者唐贵明俞鸿儒

机构地区 Institute of Mechanics

出处《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1992年第3期224-230,共7页 力学学报（英文版）

关键词 shock wave boundary layer aerodynamic heating shock wave boundary layer aerodynamic heating

分类号 O3 [理学—力学]

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参考文献14

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共引文献1

1唐贵明.SURFACE OIL FLOW TECHNIQUE AND LIQUID CRYSTAL THERMOGRAPHY FOR FLOW VISUALIZATION IN IMPULSE WIND TUNNELS[J].Acta Mechanica Sinica,1994,10(3):220-226. 被引量：1

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