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Results of tests for force, moment, pressure and aeroelastic data using the 0.030 scale pressure loads space shuttle orbiter model (47-0) in the NASA/ARC 11 foot unitary plan wind tunnel, (OA400), volume 3

机译：使用0.030比例压力载荷航天飞机轨道器模型（47-0）在Nasa / aRC 11英尺单一平面风洞（Oa400），第3卷中测试力，力矩，压力和气动弹性数据的结果

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Spangler, R. H.;
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年度 1980
页码 1-63
总页数 63
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AEROELASTICITY; FORCE DISTRIBUTION; LOADING MOMENTS; PRESSURE DISTRIBUTION; SCALE MODELS; SPACE SHUTTLE ORBITERS; WIND TUNNEL TESTS; AERODYNAMIC CONFIGURATIONS; AERODYNAMIC LOADS; STRUCTURAL DESIGN CRITERIA; WIND TUNNEL MODELS;

机译：气动弹性;力量分配;装载时刻;压力分布;尺度模型; spaCE sHUTTLE ORBITERs;风洞隧道测试;空气动力学配置;空气动力负荷;结构设计标准;风洞模型;

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1. Application of pressure-sensitive paint for determination of the pressure field and calculation of the forces and moments of models in a wind tunnel [J] . Klein C, Engler RH, Henne U, Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2005,第2期

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2. Comparison of the NASA Common Research Model European Transonic Wind Tunnel test data to NASA National Transonic Facility test data [J] . Melissa Rivers, Jürgen Quest, Ralf Rudnik CEAS Aeronautical Journal . 2018,第2期

机译：NASA通用研究模型欧洲跨音速风洞测试数据与NASA国家跨音速设施测试数据的比较
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4. Guide for Pressure-Sensitive Paint Testing at NASA Ames Research Center Unitary Plan Wind Tunnel [C] . Nettie H. Roozeboom, Jennifer K. Baerny AIAA Aerospace Sciences Meeting;AIAA SciTech Forum . 2017

机译：美国宇航局艾姆斯研究中心整体计划风洞压力敏感涂料测试指南
5. Pressure-Sensitive Paint Measurements on the NASA Common Research Model in the NASA 11-ft Transonic Wind Tunnel [O] . Bell James H. 2011

机译：NASA 11英尺跨音速风洞中基于NASA通用研究模型的压力敏感涂料测量
6. Results of tests for force, moment, pressure and aeroelastic data using the 0.030 scale pressure loads space shuttle orbiter model (47-0) in the NASA/ARC 11 foot unitary plan wind tunnel, (OA400), volume 2 [R] . Spangler, R. H. 1980

机译：使用0.030比例压力载荷航天飞机轨道器模型（47-0）在Nasa / aRC 11英尺单一平面风洞（Oa400），第2卷中测试力，力矩，压力和气动弹性数据的结果

Results of tests for force, moment, pressure and aeroelastic data using the 0.030 scale pressure loads space shuttle orbiter model (47-0) in the NASA/ARC 11 foot unitary plan wind tunnel, (OA400), volume 3

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