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A wind tunnel investigation to determine some aerodynamic hinge moments on the model engines of a saturn i, block i configuration

机译：风洞调查确定土星i的模型引擎上的一些空气动力学铰链力矩，阻止i配置

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摘要

Aerodynamic hinge moments caused by external flow on saturn i, block i nozzle configurations

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作者
Boyd, G. T.;
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年度 1963
页码 1-203
总页数 203
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
NOZZLE FLOW; SATURN 1 LAUNCH VEHICLES; STABILITY DERIVATIVES; TORQUE; WIND TUNNELS; HINGE MOMENT; NOZZLE FLOW; SATURN I LAUNCH VEHICLE;

机译：喷嘴流量; saTURN 1发射车辆;稳定性衍生物;扭矩;风洞; HINGE mOmENT;喷嘴流量; saTURN I LUNCH VEHICLE;

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2. DYNAMIC METHOD OF DETERMINING AERODYNAMIC CHARACTERISTICS OF MODELS FROM ON EXPERIMENTAL RESULTS OBTAINED IN SHORT-DURATION WIND TUNNELS [J] . A. F. Latypov Journal of Applied Mechanics and Technical Physics . 2006,第5期

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4. An improved wind tunnel configuration for the investigation of aerodynamic crosswind gust response [C] . R. G. Dominy, A. Ryan SAE International Congress and Exposition . 2000

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5. AN INVESTIGATION OF THE THEORETICAL AND EXPERIMENTAL AERODYNAMIC CHARACTERISTICS OF A LOW-CORRECTION WIND TUNNEL WALL CONFIGURATION FOR AIRFOIL TESTING. [D] . MALEK, AHMED FOUAD HASSAN. 1983

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6. Wind Tunnel Analysis of the Aerodynamic Loads on Rolling Stock over Railway Embankments: The Effect of Shelter Windbreaks [O] . Sergio Avila-Sanchez, Santiago Pindado, Oscar Lopez-Garcia, -1

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7. Investigations of the aerodynamic interactions between wind tunnel models and their support systems at the GALCIT ten foot wind tunnel [O] . Smith Josiah E. 1948

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A wind tunnel investigation to determine some aerodynamic hinge moments on the model engines of a saturn i, block i configuration

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