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Results of tests OA12 and IA9 in the Ames research center unitary plan wind tunnels of an 0.030 scale model of the space shuttle vehicle 2A to determine aerodynamic loads, volume 8

机译：测试Oa12和Ia9的结果在ames研究中心统一计划的风洞中的0.030比例模型的航天飞机车辆2a确定空气动力负荷，体积8

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For abstract, see N74-15538. For complete abstract, see .

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作者
Spangler, R. H.;
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年度 1973
页码 1-1051
总页数 1051
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC LOADS; SPACE SHUTTLES; WIND TUNNEL TESTS; ANGLE OF ATTACK; CHARTS; MACH NUMBER; PRESSURE MEASUREMENT; SPACECRAFT MODELS; SUBSONIC SPEED; SUPERSONIC SPEED; TRANSONIC SPEED;

机译：空气动力负荷;太空沙滩;风洞隧道测试;攻击角度;图;马赫数;压力测量;航天器模型; sUBsONIC spEED;超音速;跨音速;

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1. Wind tunnel testing of scaled wind turbine models: Beyond aerodynamics [J] . Carlo L. Bottasso, Filippo Campagnolo, Vlaho Petrovic Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering . 2014,第Null期

机译：比例缩放的风力涡轮机模型的风洞测试：超越空气动力学
2. Non-linear aerodynamic load and parameters estimation for a SDOF wind- structure coupling system in wind tunnel test [J] . Song Zu Lan, Hui Yi, Law Siu Seong, Engineering Structures . 2019,第Octa15期

机译：风洞试验中SDOF风固耦合系统的非线性气动载荷和参数估计
3. Development of a Wind Tunnel Test Section for Evaluation of Heavy Vehicle Aerodynamic Drag at a scale of 1:3 [J] . Damien J. McArthur, David Burton, Mark Thompson, SAE International Journal of Commercial Vehicles . 2013,第2期

机译：开发风洞试验段以评估1：3的重型车辆空气阻力
4. Space Launch System Booster Separation Aerodynamic Testing in the NASA Langley Unitary Plan Wind Tunnel [C] . Floyd J. Wilcox Jr., Jeremy T. Pinier, David T. Chan, AIAA aerospace sciences meeting;AIAA SciTech Forum . 2016

机译：NASA兰利单一计划风洞中的太空发射系统助推器分离空气动力学测试
5. 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

Results of tests OA12 and IA9 in the Ames research center unitary plan wind tunnels of an 0.030 scale model of the space shuttle vehicle 2A to determine aerodynamic loads, volume 8

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