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Comparison of wind-tunnel and flight test aerodynamic data in the transition-flight speed range for five V/STOL aircraft

机译：五架V / sTOL飞机在过渡飞行速度范围内的风洞和飞行试验空气动力学数据的比较

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V/STOL wind tunnel model and flight test vehicle aerodynamic characteristics comparison

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作者
Cook, W. L.; Hickey, D. H.;
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年度 1966
页码 1-21
总页数 21
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; AERODYNAMICS; AIRCRAFT MODELS; ANGLE OF ATTACK; COMPARISON; CONFERENCES; FLIGHT TEST VEHICLES; FLIGHT TESTS; RATES (PER TIME); SHORT TAKEOFF AIRCRAFT; TRANSITION FLIGHT; V/STOL AIRCRAFT; WIND TUNNEL MODELS; WIND TUNNEL TESTS; AERODYNAMIC CHARACTERISTICS; FLIGHT TEST VEHICLE; V/STOL AIRCRAFT; WIND TUNNEL MODEL;

机译：空气动力学特征;空气动力学;飞机模型;攻击角度;比较;大会;飞行测试车辆;飞行测试;费率（每次）;短途飞机;过渡飞行; V / sTOL aIRCRaFT;风洞模型;风洞隧道测试;空气动力学特征;飞行试验车; V / sTOL aIRCRaFT;风洞模型;

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1. Comparison of flight test data with a computational fluid dynamics model of a Scottish Aviation Bulldog aircraft [J] . N. J. Lawson, N. Salmon, J. E. Gautrey, The Aeronautical Journal . 2013,第1198期

机译：飞行测试数据与苏格兰航空斗牛犬飞机的计算流体动力学模型的比较
2. Comparison Study and Sensitivity Analysis of Flight Test Techniques for Air Data Position Error Correction in Small Aircraft [J] . Sang-Jong Lee, Jae Won Chang, Jeong Ho Park, Transactions of the Japan society for aeronautical and space sciences . 2011,第182期

机译：小型飞机空中数据位置误差校正飞行测试技术的对比研究与敏感性分析
3. Comparisons of computational fluid dynamics solutions of static and manoeuvring fighter aircraft with flight test data [J] . D R McDaniel, R M Cummings, K Bergeron, Proceedings of the Institution of Mechanical Engineers . 2009,第g4期

机译：静态和机动战斗机的计算流体动力学解决方案与飞行测试数据的比较
4. Aircraft aerodynamic coefficients identification using flight tests data [C] . O N Korsun, A V Stulovskii, O A Balyk Workshop on materials and engineering in aeronautics . 2018

机译：飞机空气动力系数使用飞行测试数据识别
5. DETERMINATION OF AERODYNAMIC AND PROPULSION PARAMETERS OF GENERAL AVIATION AIRCRAFT USING STEADY STATE FLIGHT TEST DATA. [D] . SABZEHPARVAR, MEHDI. 1984

机译：使用稳态飞行测试数据确定通用航空飞机的气动和推进参数。
6. Aerodynamics of a highly irregular body at transonic speeds—Analysis of STRATOS flight data [O] . Markus Guerster, Ulrich Walter 2011

机译：跨音速下高度不规则物体的空气动力学— STRATOS飞行数据分析
7. Flight testing a V/STOL aircraft to identify a full-envelope aerodynamic model [O] . Mcnally, B. David, Bach, Ralph E., Jr. 1988

机译：对V / STOL飞机进行飞行测试以识别全信封空气动力学模型

Comparison of wind-tunnel and flight test aerodynamic data in the transition-flight speed range for five V/STOL aircraft

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