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Pressure and heat-transfer distributions of 0.1-scale Gemini exit and reentry models at Mach numbers of 3.51 and 4.44

机译：0.1级Gemini出口和再入模型的压力和传热分布在马赫数为3.51和4.44时

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作者
Howard, P. W.; Stallings, R. L., Jr.; Howard, P. W.;
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年度 1965
页码 1-110
总页数 110
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
GEMINI SPACECRAFT; HEAT TRANSFER; PRESSURE DISTRIBUTION; TEMPERATURE DISTRIBUTION; MANNED REENTRY; SUPERSONIC FLOW;

机译：GEmINI spaCECRaFT;传播热量;压力分布;温度分布; mannED REENTRY;超音速流;

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Pressure and heat-transfer distributions of 0.1-scale Gemini exit and reentry models at Mach numbers of 3.51 and 4.44

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