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AN INVESTIGATION OF FLOW VISUALIZATION TECHNIQUES IN HELIUM AT MACH NUMBERS OF 15 AND 20

机译：氦在15和20机械数下的流动可视化技术研究

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摘要

Flow visualization techniques in helium at mach 15 & 20 - surface streamlines, attached and separated afterbody flow & stagnation points

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作者
Duller, C. E.;
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年度 1963
页码 1-18
总页数 18
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AFTERBODIES; ANGLE OF ATTACK; BOUNDARY LAYER SEPARATION; FLOW VISUALIZATION; HELIUM; HYPERSONIC FLOW; MACH NUMBER; SEPARATED FLOW; STAGNATION POINT; FLOW SEPARATION; FLOW VISUALIZATION; HELIUM; HYPERSONIC FLOW; STAGNATION POINT;

机译：aFTERBODIEs;攻击角度;边界层分离;流动可视化;氦;超音速流动;马赫数;分离流量; sTaGNaTION pOINT;流动分离;流动可视化;氦;超音速流动; sTaGNaTION pOINT;

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5. Experimental pressure and heat transfer investigation over a "directed-energy air spike" inlet at flow mach numbers of 10 to 20, stagnation temperature of 1000 K, and arc powers up to 127 KW. [D] . Toro, Paulo Gilberto de Paula. 1998

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AN INVESTIGATION OF FLOW VISUALIZATION TECHNIQUES IN HELIUM AT MACH NUMBERS OF 15 AND 20

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