首页> 美国政府科技报告 >Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B orbiter configuration (model 47-0) in the 11-foot unitary plan wind tunnel for Mach 0.6 and 0.9 (0A22A)

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Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B orbiter configuration (model 47-0) in the 11-foot unitary plan wind tunnel for Mach 0.6 and 0.9 (0A22A)

机译：airloads调查了一架0.030比例的航天飞机车辆140a / B轨道飞行器配置（型号47-0）在11英尺单一平面风洞中的测量值为0.6和0.9马赫（0a22a）

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For abstract, see N75-23647.

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作者
Gillins, R. L.;
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年度 1975
页码 1-709
总页数 709
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LAUNCH VEHICLE CONFIGURATIONS; SPACE SHUTTLE ORBITERS; WIND TUNNEL MODELS; WIND TUNNEL TESTS; AERODYNAMIC LOADS; ANGLE OF ATTACK; PRESSURE DISTRIBUTION; SIDESLIP; SPACE SHUTTLE BOOSTERS; SUBSONIC SPEED; WING TANKS;

机译：发射车辆配置; spaCE sHUTTLE ORBITERs;风洞模型;风洞隧道测试;空气动力负荷;攻击角度;压力分布;侧滑; spaCE sHUTTLE BOOsTERs; sUBsONIC spEED; WING TaNKs;

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1. Fluid mechanics of a Mach 7-12, electron-beam driven, missile-scale hypersonic wind tunnel: Modeling and predictions [J] . Girgis IG., Brown GL., Miles RB., Physics of fluids . 2002,第11期

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2. Study of the Wind Tunnel Effect on the Drag Coefficient (C_D) of a Scaled Static Vehicle Model Compared to a Full Scale Computational Fluid Dynamic Model [J] . Sanwar A. Sunny Asian Journal of Scientific Research . 2011,第3期

机译：风洞对比例静态车辆模型与全比例计算流体动力学模型的阻力系数（C _{D ）的影响研究}
3. Model vehicle movement system in wind tunnels for exhaust dispersion studies under various urban street configurations [J] . K. Ahmad, M. Khare, K. K. Chaudhry Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2002,第9期

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4. A Preliminary Investigation of the Check Standard Model in the NASA Ames Unitary Plan Wind Tunnel [C] . Max Amaya, Ross Flach, Theodore J. Garbeff Ⅱ AIAA aviation forum . 2019

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5. Flow-field measurements in the windward surface shock layer of space shuttle orbiter configurations at Mach number 8 [O] . Carter, L. D., Martindale, W. R. 1975

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Airloads investigation of an 0.030 scale model of the space shuttle vehicle 140A/B orbiter configuration (model 47-0) in the 11-foot unitary plan wind tunnel for Mach 0.6 and 0.9 (0A22A)

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