首页> 美国政府科技报告 >Results of tests using a 0.02 scale model (105-0) of the space shuttle vehicle orbiter in the Arnold Engineering Development Center Von Karman Facility supersonic tunnel A(OA209) and hypersonic tunnel B (OA208)

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Results of tests using a 0.02 scale model (105-0) of the space shuttle vehicle orbiter in the Arnold Engineering Development Center Von Karman Facility supersonic tunnel A(OA209) and hypersonic tunnel B (OA208)

机译：在arnold工程开发中心Von Karman设施超音速隧道a（Oa209）和高超声速隧道B（Oa208）中使用0.02比例模型（105-0）的航天飞机车辆轨道器的测试结果

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Daileda, J. J.;
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年度 1979
页码 1-1107
总页数 1107
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
SCALE MODELS; SPACE SHUTTLE ORBITERS; SPACE SHUTTLES; SPACECRAFT CONTROL; WIND TUNNEL TESTS; FLOW DISTRIBUTION; HYPERSONIC SPEED; HYPERSONIC WIND TUNNELS; PITCH (INCLINATION); SPACECRAFT STABILITY; SUPERSONIC SPEED; SUPERSONIC WIND TUNNELS; YAW;

机译：尺度模型; spaCE sHUTTLE ORBITERs;太空沙滩;航天器控制;风洞隧道测试;流量分配;超速的;超级风洞; pITCH（倾斜）;航天器稳定性;超音速;超级风洞;偏航;
入库时间 2022-08-29 11:09:45

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1. Hot paints - A team from Arnold Engineering Development Center has been using Temperature Sensitive Paint (TSP) in the unique Wind Tunnel 9 to obtain heat data for Orion's Crew Exploration Vehicle (CEV) [J] . Philip Lorenz III Aerospace Testing International . 2007,第3期

机译：热涂料-阿诺德工程开发中心的一个团队一直在独特的风洞9中使用温度敏感涂料（TSP）来获取猎户座乘员探索车（CEV）的热量数据
2. SUBSONIC FACILITY - SUPERSONIC STEAM TUNNEL, VIBRATIONS FACILITY, PYROTECHNICAL SHOCK TEST FOR SPACE EQUIPMENT [J] . Decuypere R, Baudoin Y, Bourgois R, European Journal of Mechanical and Environmental Engineering . 1995,第3期

机译：亚音速设施-超音速蒸汽隧道，振动设施，空间设备的烟火冲击试验
3. Arnold Engineering Development Center (AEDC) Hypervelocity Wind Tunnel 9 [J] . Dan Marren The ITEA Journal of Test and Evaluation . 2007,第2期

机译：阿诺德工程开发中心（AEDC）超高速风洞9
4. Arnold Engineering Development Complex Von Karman Facility Hypersonic Wind Tunnels [C] . Michael L. Mills AIAA SciTech forum;AIAA Aerospace Sciences Meeting . 2015

机译：阿诺德工程开发综合体冯卡曼设施高超音速风洞
5. Initial Assessment of Acoustic Source Visibility with a 24-Element Microphone Array in the Arnold Engineering Development Center 80- by 120-Foot Wind Tunnel at NASA Ames Research Center [O] . Horne William C. 2011

机译：在美国宇航局艾姆斯研究中心的Arnold工程开发中心80 x 120英尺风洞中使用24元素麦克风阵列对声源能见度进行初步评估
6. Results of heat transfer tests in the Arnold Engineering Development Center: von Karman facility tunnels A and B utilizing Space Shuttle orbiter thin skin thermocouple models 56-0, 60-0 and 83-0: Volume 1: Tests: OH-84B, OH-105, IH-102 [R] . Foust, J. W. 1981

机译：阿诺德工程开发中心的传热测试结果：von Karman设施隧道a和B利用航天飞机轨道飞行器薄皮热电偶模型56-0,60-0和83-0：第1卷：测试：OH-84B，OH- 105，IH-102

Results of tests using a 0.02 scale model (105-0) of the space shuttle vehicle orbiter in the Arnold Engineering Development Center Von Karman Facility supersonic tunnel A(OA209) and hypersonic tunnel B (OA208)

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