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Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6

机译：马赫数为6的高超声速传输模型的气动特性研究

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Wind tunnel investigation of hypersonic transport model aerodynamic characteristics at Mach numbers to 6 - graphs

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作者
Ellison, J. C.;
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年度 1971
页码 1-80
总页数 80
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; BODY-WING AND TAIL CONFIGURATIONS; HYPERSONIC SPEED; SUBSONIC SPEED; SUPERSONIC SPEED; GRAPHS (CHARTS); WIND TUNNEL MODELS;

机译：空气动力学特征;身体和尾部的配置;超速的; sUBsONIC spEED;超音速;图表（图表）;风洞模型;

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专利

1. NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION [J] . S. M. Zadonsky, A. P. Kosykh, G. G. Nersesov, TsAGI science journal . 2013,第1期

机译：一体化结构超音速飞机模型气动特性的数值和实验研究
2. Investigation of hypersonic inlet pulse-starting characteristics at high Mach number [J] . Jiao Xiaoliang, Chang Juntao, Wang Zhongqi, Aerospace science and technology . 2016,第NOVa期

机译：高马赫数高超声速进气脉冲启动特性研究
3. INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF A HYPERSONIC FLOW AROUND BODIES OF REVOLUTION WITH A PERMEABLE TIP [J] . N. I. Sidnyaev Journal of Applied Mechanics and Technical Physics . 2007,第2期

机译：带有尖端的超音速绕流旋转机构的气动特性研究
4. Experimental Investigations of an Aerodynamic Flow of Geometrical Models in Hypersonic Aerodynamic Shock Tube [C] . M.A. Kotov, I.A. Kryukov, L.B. Ruleva, AIAA applied aerodynamics conference . 2013

机译：高超音速气动冲击管中几何模型气动流动的实验研究
5. Unsteady aerodynamic modeling with time-varying free-stream Mach numbers. [D] . Jose, Arun Isaac. 2005

机译：随时间变化的自由流马赫数的非定常空气动力学建模。
6. Aerodynamic Characteristics of a Stoker Furnace withStaged Combustion: Comparison of Cold Modeling Experiments and NumericalSimulations [O] . Xinwei Guo, Hao Bai, Zhongxiao Zhang, 2020

机译：炉膛空气动力学特性分阶段燃烧：冷建模实验与数值比较模拟
7. Aerodynamic characteristics of a wedge and cone at hypersonic mach numbers. [O] . De Lauer Richard D. 1950

机译：高超声速马赫数下楔形和圆锥形的空气动力学特性。
8. Investigation of the Aerodynamic Characteristics of a Hypersonic Transport Model at Mach Numbers to 6 [R] . Ellison, J. C. 1971

机译：高速传输模型在马赫数为6时的气动特性研究

Investigation of the aerodynamic characteristics of a hypersonic transport model at Mach numbers to 6

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