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Reversibility Theorem for Thin Airfoils in Subsonic and Supersonic Flow.

机译：可逆性定理薄翼型在亚音速和超音速。

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NO ABSTRACT DUE TO ILLEGIBILITY OF REPORT.

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作者
Brown, C. E.;
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年度 1950
页码 1-8
总页数 8
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Airfoils; Reversible; Subsonic flow; Supersonic flow; Thinness; Theorems; Reversibility theorem;

机译：翼型件;可逆的;亚音速流;超音速流;瘦;定理;可逆性定理;

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专利

1. ASYMPTOTIC SOLUTION OF THE PROBLEM OF A SUBSONIC GAS FLOW AROUND AN AIRFOIL WITH A LOCAL SUPERSONIC AREA FORMATION [J] . A. V. Zubtsov, G. G. Soudakov TsAGI science journal . 2011,第2期

机译：局部超音速形成的翼型周围亚音速气流问题的渐近解
2. ON THE AERODYNAMIC CHARACTERISTICS OF A CLASS OF AIRFOILS WITH CONTINUOUS CURVATURE AT SUBSONIC, TRANSONIC AND SUPERSONIC REGIMES [J] . C. BERBENTE, S. DANAILA University Politechnica of Bucharest scientific bulletin, D. Mechanical Engineering . 2007,第1期

机译：亚音速，超音速和超音速连续翼型的气动特性
3. Subsonic/supersonic yawed gust over an airfoil [J] . Paulo A.O.Soviero, Hugo B.Resende AIAA Journal . 1997,第2期

机译：亚音速/超音速在机翼上偏航
4. Low Frequency Oscillations Of Thin Airfoils In Subsonic Compressible Flows [C] . D. Mateescu, S. Neculita AIAA Aerospace Sciences Meeting and Exhibit . 2006

机译：亚音速可压缩流中薄翼型的低频振荡
5. Computational analysis of blunt, thin airfoil sections at supersonic and subsonic speeds. [D] . Goodsell, Aga Myung. 2002

机译：在超音速和亚音速下进行钝性薄翼型截面的计算分析。
6. The transition from subsonic to supersonic cracks [O] . Chris Behn, M. Marder -1

机译：从亚音速到超音速裂纹的过渡
7. Improved numerical method for lifting airfoils with oscillating control surfaces in subsonic flow. [O] . Akio ICHIKAWA 1985

机译：提高亚音流振荡控制表面提升翼型的数值方法。

Reversibility Theorem for Thin Airfoils in Subsonic and Supersonic Flow.

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