首页> 美国政府科技报告 >Results of tests on a .02 scale space shuttle launch vehicle model (89OTS) in the LARC 16 ft transonic wind tunnel to determine pressure distribution along the external tank LOX cable tray (LA132)

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Results of tests on a .02 scale space shuttle launch vehicle model (89OTS) in the LARC 16 ft transonic wind tunnel to determine pressure distribution along the external tank LOX cable tray (LA132)

机译：LaRC 16英尺跨音速风洞中的.02比例航天飞机运载火箭模型（89OTs）测试结果，以确定沿外部水箱LOX电缆桥架（La132）的压力分布

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年度 1980
页码 1-811
总页数 811
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
EXTERNAL TANKS; PRESSURE DISTRIBUTION; SCALE MODELS; SPACE SHUTTLE ASCENT STAGE; SPACE SHUTTLE BOOSTERS; WIND TUNNEL TESTS; AERODYNAMIC CHARACTERISTICS; LIQUID OXYGEN; TABLES (DATA); TRANSONIC SPEED; TRANSONIC WIND TUNNELS; WIND TUNNEL MODELS;

机译：外部坦克;压力分布;尺度模型;空间穿梭阶段; spaCE sHUTTLE BOOsTERs;风洞隧道测试;空气动力学特征;液体氧气;表（数据）;跨音速;跨音风洞;风洞模型;

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1. Estimation of the Unsteady Aerodynamic Load on Space Shuttle External Tank Protuberances from a Component Wind Tunnel Test [C] . J. Panda, F. Martin, D. Sutcliff AIAA Aerospace Sciences Meeting and Exhibit . 2008

机译：从组件风洞试验估算航天飞机外部储罐突出部分上的非稳态气动载荷
2. Estimation of the Unsteady Aerodynamic Load on Space Shuttle External Tank Protuberances from a Component Wind Tunnel Test [O] . Sutliff Daniel L., Panda Jayatana, Martin Fred W. 2008

机译：从组件风洞试验估算航天飞机外部储罐突出部分的非稳态气动载荷
3. Results of the space shuttle vehicle ascent air data system probe calibration test using a 0.07-scale external tank forebody model (68T) in the AEDC 16-foot transonic wind tunnel (IA-310), volume 1 [R] . Collette, J. G. R. 1991

机译：在aEDC 16英尺跨音速风洞（Ia-310）中使用0.07比例外部坦克前体模型（68T）的航天飞机车辆上升空气数据系统探测器校准测试结果，第1卷

Results of tests on a .02 scale space shuttle launch vehicle model (89OTS) in the LARC 16 ft transonic wind tunnel to determine pressure distribution along the external tank LOX cable tray (LA132)

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