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Results of a wind tunnel pressure loads test of the 0.03-scale Space Shuttle Orbiter (model 47-0) in the 8 x 7 foot leg of the NASA/ARC unitary plan wind tunnel (OA146), volume 2

机译：美国国家航空航天局/ aRC单一平面风洞（Oa146）8 x 7英尺长的0.03级航天飞机轨道器（型号47-0）的风洞压力负荷试验结果，第2卷

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Marroquin, J.;
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年度 1983
页码 1-56
总页数 56
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AEROTHERMODYNAMICS; PRESSURE DISTRIBUTION; SPACE SHUTTLE ORBITERS; WIND TUNNEL TESTS; ABORTED MISSIONS; HYPERSONIC FORCES; SCALE MODELS; STABILITY DERIVATIVES; TABLES (DATA);

机译：气动热力学;压力分布; spaCE sHUTTLE ORBITERs;风洞隧道测试;被迫出任的使命;超级力量;尺度模型;稳定性衍生物;表（数据）;

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8. Results of a wind tunnel pressure loads test of the 0.03-scale space shuttle orbiter (model 47-0) in the 8x7-foot leg of the NASA/ARC unitary plan wind tunnel (OA146), volume 1 [R] . Marroquin, J. 1983

机译：美国宇航局/ aRC单一计划风洞（Oa146）8x7英尺长的0.03级航天飞机轨道器（型号47-0）的风洞压力负荷试验结果，第1卷

Results of a wind tunnel pressure loads test of the 0.03-scale Space Shuttle Orbiter (model 47-0) in the 8 x 7 foot leg of the NASA/ARC unitary plan wind tunnel (OA146), volume 2

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