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Pressure distributions on blunt delta wings at a Mach number of 2.91 and angles of attack up to 90 deg

机译：钝齿三角翼上的压力分布，马赫数为2.91，迎角高达90度

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作者
Mueller, J. N.;
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年度 1962
页码 1-116
总页数 116
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
AERODYNAMIC CHARACTERISTICS; BLUNT BODIES; DELTA WINGS; PRESSURE DISTRIBUTION; WIND TUNNEL MODELS; ANGLE OF ATTACK; MACH NUMBER; SUPERSONIC WIND TUNNELS;

机译：空气动力学特征; BLUNT BODIEs; DELTa WINGs;压力分布;风洞模型;攻击角度;马赫数;超级风洞;

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1. Surface pressure model for simple delta wings at high angles of attack [J] . A. A. Pashilkar Sadhana: Academy Proceedings in Engineering Science . 2001 ,第6期

机译：高攻角下简单三角翼的表面压力模型
2. Aerodynamic Characteristics of a Delta Wing in the Case of Harmonic Oscillations with Respect to the Roll and Yaw Angles at High Angles of Attack [J] . E. A. Karavaev, E. A. Chasovnikov Fluid Dynamics . 2013 ,第2期

机译：相对于大迎角的侧倾角和横摆角，在谐波振荡情况下三角翼的空气动力学特性
3. Effects of Angle of Attack and Bluntness on Heating Rate Distribution of Blunt Models at Hypersonic Speeds [J] . Fluid Dynamics . 2019 ,第6期

机译：攻击角度与钝化对高音速度钝化模型加热速率分布的影响
4. CFD Predictions of Wing Pressure Distributions on the F- 35 at Angles- of- Attack for Transonic Maneuvers [C] . P. Wooden, B. Smith, J. Azevedo AIAA Applied Aerodynamics Conference . 2007

机译：跨音速机动的F-35迎角迎角分布的CFD预测
5. Modeling the rolling moment on the 65-degree delta wing for rolling motions at high angle of attack. [D] . Myatt, James Harold. 1997

机译：对65度三角翼上的侧倾力矩进行建模，以实现高攻角下的侧倾运动。
6. Association of quadriceps angle with plantar pressure distribution navicular height and calcaneo-tibial angle [O] . Ata Elvan, Ibrahim Engin Simsek, Mehmet Alphan Cakiroglu, 2019

机译：股四头肌角与足底压力分布鼻高和胫腓骨角的关系
7. NUMERICAL ANALYSIS OF PRESSURE PERTURBATION OF DELTA WING VORTEX FLOW AT A HIGH ANGLE OF ATTACK [O] . M.S. Son, J.H. Sa, S.H. Park, 2015

机译：高攻角δ翼涡流压力扰动的数值分析
8. Pressure distributions on a flat-plate delta wing swept 65 deg at a Mach number of 5.97 at angles of attack from 65 deg to 115 deg and angles of roll from 0 deg to 25 deg at a 90 deg angle of attack [R] . Goldberg, T. J., Hondros, J. G. 1962

机译：平板三角翼上的压力分布以65度的攻角从65度到115度以及从0度到25度的角度在90度迎角下以马赫数5.97扫描65度

Pressure distributions on blunt delta wings at a Mach number of 2.91 and angles of attack up to 90 deg

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