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A study of local-pressure fluctuations relative to static-pressure distributions on two-dimensional airfoils at high subsonic Mach numbers

机译：高亚音速马赫数下二维翼型相对于静压分布的局部压力波动研究

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Coe, Charles F;
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年度 1955
页码 1-68
总页数 68
原文格式 PDF
正文语种 eng
中图分类工业技术;
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专利

1. Study of the conditions that cause chaotic motion in a two-dimensional airfoil with structural nonlinearities in subsonic flow [J] . D. Li, S. Guo, J. Xiang Journal of Fluids and Structures . 2012,第Null期

机译：亚音速流中具有结构非线性的二维翼型中引起混沌运动的条件的研究
2. Effect of mach number on high-subsonic and low-Reynolds-number flows around airfoils [J] . International Journal of Modern Physics, B. Condensed Matter Physics, Statistical Physics, Applied Physics . 2020,第14a16期

机译：Mach数对翼型的高次级和低雷诺数流动的影响
3. Increase of Critical Mach Number by Local Linearization Method and Airfoil Construction at Subsonic and Transonic Regimes [J] . Bazgir Ali. S., Takovitskii Sergey. A. MATEC Web of Conferences . 2018,第期

机译：亚态和跨音质制度的局部线性化方法和翼型施工的临界机械数量增加
4. Transition studies on a two-dimensional NACA63 isolated airfoil at high mach numbers [C] . S Svensdotter, j Hu, T Fransson European conference on turbomachinery . 1999

机译：高马赫数二维NACA63分离机翼的过渡研究
5. Aerodynamic performance of transonic and subsonic airfoils: Effects of surface roughness, turbulence intensity, Mach number, and streamline curvature-airfoil shape. [D] . Zhang, Qiang. 2005

机译：跨音速和亚音速机翼的空气动力学性能：表面粗糙度，湍流强度，马赫数和流线曲率翼型的影响。
6. The effect of pore size and density on ultrasonic attenuation in porous structures with mono-disperse random pore distribution: A two-dimensional in-silico study [O] . Omid Yousefian, R. D. White, Yasamin Karbalaeisadegh, -1

机译：孔径和密度对具有单分散随机孔分布的多孔结构中超声衰减的影响：二维硅树脂研究
7. Increase of Critical Mach Number by Local Linearization Method and Airfoil Construction at Subsonic and Transonic Regimes [O] . Ali. S. Bazgir, Sergey. A. Takovitskii 2018

机译：亚态和跨音质制度的局部线性化方法和翼型施工的临界机械数量增加

A study of local-pressure fluctuations relative to static-pressure distributions on two-dimensional airfoils at high subsonic Mach numbers

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