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Data report of 0.055-scale Apollo dynamic stability model /FD-2/ tests to determine flow separator effects, high Mach leg of the Langley unitary plan wind tunnel /project 411/

机译：0.055比例的apollo动态稳定性模型/ FD-2的数据报告/确定流动分离器效应的测试，Langley单一计划风洞/项目的高马赫腿411 /

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作者
Berthold, C. L.; Mitchell, C. E.;
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年度 1963
页码 1-41
总页数 41
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
APOLLO SPACECRAFT; WIND TUNNEL MODELS; WIND TUNNEL STABILITY TESTS; AERODYNAMIC CHARACTERISTICS; SPACECRAFT PERFORMANCE; SPACECRAFT STABILITY;

机译：apOLLO spaCECRaFT;风洞模型;风洞稳定性试验;空气动力学特征;航天器性能;航天器稳定性;

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1. 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

机译：NASA兰利单一计划风洞的超音速反推进动态数据分析
2. Modelica-based dynamic analysis and design of lift-generating disk-type wind blade using computational fluid dynamics and wind tunnel test data [J] . Yoo Yeongmin, Lee Soyoung, Yoon Jaehyun, Mechatronics: The Science of Intelligent Machines . 2018,第期

机译：基于ModelICA的动态分析和设计利用计算流体动力学和风洞测试数据的提升盘式风刀
3. WindSim? Computational Flow Dynamics Model Testing Using Databases from Two Wind Measurement Stations [J] . ?or?e Klisi?, Miodrag Zlatanovi?, Ilija Radovanovi? Elektronika . 2011,第2期

机译：WindSim？使用来自两个测风站的数据库进行的计算流动动力学模型测试
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

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5. The effect of systematic error in forced oscillation wind tunnel test apparatuses on determining nonlinear unsteady aerodynamic stability derivatives. [D] . Williams, Brianne Y. 2010

机译：强制振荡风洞测试设备中的系统误差对确定非线性非稳态气动稳定性导数的影响。
6. ARES I Aerodynamic Testing at the NASA Langley Unitary Plan Wind Tunnel [O] . Wilcox Floyd J., Erickson Gary E. 2011

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7. Data report for Langley unitary plan wind tunnel tests /project 349/ of Apollo Model /FD-2/ [R] . 1962

机译：兰利单一计划风洞试验/项目349 / apollo model / FD-2 /的数据报告

Data report of 0.055-scale Apollo dynamic stability model /FD-2/ tests to determine flow separator effects, high Mach leg of the Langley unitary plan wind tunnel /project 411/

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