首页> 美国政府科技报告 >Results of aerothermodynamic heat transfer tests on a 0.03-scale model (93-0) simulating the elevon/elevon gap and elevon/fuselage interface regions of the Space Shuttle Orbiter in the Ames Research Center 3.5-foot hypersonic wind tunnel (QH58)

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Results of aerothermodynamic heat transfer tests on a 0.03-scale model (93-0) simulating the elevon/elevon gap and elevon/fuselage interface regions of the Space Shuttle Orbiter in the Ames Research Center 3.5-foot hypersonic wind tunnel (QH58)

机译：模拟ames研究中心3.5英尺高超音速风洞（QH58）中航天飞机轨道器的升高/升高间隙和升降/机身界面区域的0.03比例模型（93-0）的气动热传导试验结果

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Kingsland, R. B.;
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年度 1979
页码 1-289
总页数 289
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC HEAT TRANSFER; AEROTHERMODYNAMICS; HYPERSONIC HEAT TRANSFER; SPACE SHUTTLE ORBITERS; WIND TUNNEL TESTS; DATA REDUCTION; ELEVONS; FLAT PLATES; FUSELAGES; HYPERSONIC SPEED; HYPERSONIC WIND TUNNELS; PRESSURE; SCALE MODELS; TEST FACILITIES; THERMOCOUPLES;

机译：空气动力传热;气动热力学;超音速换热; spaCE sHUTTLE ORBITERs;风洞隧道测试;数据减少;升降副翼;平板;机身;超速的;超级风洞;压力;尺度模型;测试设施;热电偶;

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1. Aerodynamic heating tests of a 0.10 scale Space Shuttle orbiter elevon/elevon gap model 93-0 in the NASA/ARC 3.5 foot hypersonic wind tunnel (OH108) [R] . Gee, J. 1982

机译：Nasa / aRC 3.5英尺高超音速风洞（OH108）中0.10级航天飞机轨道器升力/升高间隙模型93-0的空气动力学加热试验

Results of aerothermodynamic heat transfer tests on a 0.03-scale model (93-0) simulating the elevon/elevon gap and elevon/fuselage interface regions of the Space Shuttle Orbiter in the Ames Research Center 3.5-foot hypersonic wind tunnel (QH58)

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