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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 8x7-foot leg of the NASA/ARC unitary plan wind tunnel (OA146), volume 1

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

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Marroquin, J.;
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年度 1983
页码 1-471
总页数 471
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AEROTHERMODYNAMICS; PRESSURE DISTRIBUTION; SCALE MODELS; SPACE SHUTTLE ORBITERS; WIND TUNNEL TESTS; ABORTED MISSIONS; AERODYNAMIC LOADS; ANGLE OF ATTACK; HYPERSONIC SPEED; TABLES (DATA); WINGS;

机译：气动热力学;压力分布;尺度模型; spaCE sHUTTLE ORBITERs;风洞隧道测试;被迫出任的使命;空气动力负荷;攻击角度;超速的;表（数据）; WINGs;

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2. Supersonic Retropropulsion Validation Experiment in the NASA Langley Unitary Plan Wind Tunnel [J] . Scott A. Berry, Matthew N. Rhode, Karl Edquist Journal of Spacecraft and Rockets . 2014,第3期

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3. Supersonic Retropropulsion Dynamic Data Analysis from NASA Langley Unitary Plan Wind Tunnel [J] . Joshua R. Codoni, Scott A. Berry Journal of Spacecraft and Rockets . 2014,第3期

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5. Pressure distribution on the roof of a model low-rise building tested in a boundary layer wind tunnel. [D] . Goliber, Matthew Robert. 2009

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6. Wind Tunnel Tests for Wind Pressure Distribution on Gable Roof Buildings [O] . Xiao-kun Jing, Yuan-qi Li 2013

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7. 1 Testing of the Crew Exploration Vehicle in NASA Langley’s Unitary Plan Wind Tunnel [O] . Daniel R. Cole, Richard J. Schwartz 2014

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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 8 x 7 foot leg of the NASA/ARC unitary plan wind tunnel (OA146), volume 2 [R] . Marroquin, J. 1983

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

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

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