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Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at mach numbers of 1.41, 2.01, and 6.86

机译：在1.41,2.01和6.86的马赫数下，前体绞车对高超音速飞机结构的俯仰和侧滑的气动特性的影响

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Effect of forebody strakes on aerodynamic characteristics in sideslip and pitch of hypersonic aircraft configurations

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作者
Driver, C.;
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年度 1959
页码 1-48
总页数 48
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
AERODYNAMIC CHARACTERISTICS; AIRCRAFT CONFIGURATIONS; ANGLE OF ATTACK; FOREBODIES; HYPERSONIC AIRCRAFT; HYPERSONICS; MACH NUMBER; PITCH (INCLINATION); SIDESLIP; STRAKES; AERODYNAMIC CHARACTERISTICS; FOREBODY; HYPERSONIC AIRCRAFT; PITCH ATTITUDE; SIDESLIP;

机译：空气动力学特征;飞机配置;攻击角度; FOREBODIEs;超音速飞机;高超声速;马赫数; pITCH（倾斜）;侧滑;边条;空气动力学特征;船首;超音速飞机; pITCH aTTITUDE;侧滑;

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专利

1. Forebody Strake Effects on Rocket Aerodynamic Characteristics at High Angles of Attack [J] . William V. Logan, Roger L. Davis, Nesrin Sarigul-Klijn, Journal of Spacecraft and Rockets . 2008 ,第4期

机译：高攻角时前体风向对火箭气动特性的影响
2. Aerodynamic characteristics of breathing blunt nose configuration at hypersonic speeds [J] . Watanabe Yasumasa, Suzuki Kojiro, Rathakrishnan Ethirajan Proceedings of the Institution of Mechanical Engineers . 2017 ,第G5期

机译：超音速下呼吸钝鼻构造的空气动力学特征
3. 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
4. Effect of Forebody Strake on Directional Aerodynamic Characteristics of Typical Configuration and its Mechanism [C] . Yankui Wang, Bingrui Fu, Shuai Ou ASME Fluids Engineering Division Meeting . 2014

机译：前置面对典型配置的方向空气动力学特性的影响及其机制
5. Aerodynamics of a chined forebody oscillating in pitch. [D] . Mange, Richard Lewis. 1996

机译：下巴前倾的气动特性。
6. A Conceptual Design of Next Generation Hypersonic Air-breathing Airplanes with Dual Waveriders Forebody [O] . Kai Cui, Shouchao Hu, Guangli Li, 2015

机译：下一代超音速空气呼吸飞机的概念设计与双波机前器

Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at mach numbers of 1.41, 2.01, and 6.86

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