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Transitional Characteristics of Vortices Issued From A Body Which Creates Asymmetric Flow Field. In A Case of Thin Symmetrical Airfoil With Angle of Attack Under Rotational Oscillation of Small Amplitude.

机译：从创造非对称流场发出的涡流的过渡特征。在较小振幅的旋转振荡下具有呈现角度的薄对称翼型的情况。

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Hiroyuki HANIU; Hiroshi SAKAMOTO; Yoshihiro OBATA; Takashi SHIRAGA;
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年度 1992
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1. Asymmetric Vortices Around a Body in a High angle of attack Supersonic Flow [J] . Mee-Young PARK, Wan-Sub KIM, Sangho KIM, Journal of the Korean Physical Society . 2009,第5aPta2期

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2. ASYMMETRIC VORTICES FLOW OVER SLENDER BODY AND ITS ACTIVE CONTROL AT HIGH ANGLE OF ATTACK [J] . DENG Xueying, WANG Yankui 力学学报：英文版 . 2004,第006期

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3. A physical model of asymmetric vortices flow structure in regular state over slender body at high angle of attack [J] . DENG Xueying, WANG Gang, CHEN Xuerui, Science in China. Series E, Technological sciences . 2003,第6期

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4. Study of asymmetric vortices over a slender body of revolution at high angles of attack [C] . A. Larabi, K. Knowles, A . J. Saddington Advanced aerodynamics conference 2014: Advanced aero concepts, design and operations . 2014

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5. An experimental investigation of the physical mechanisms controlling the asymmetric flow past slender bodies at large angles of attack. [D] . Moskovitz, Cary A. 1989

机译：实验研究了在大迎角下控制不对称流动通过细长体的物理机制。
6. Flutter characteristics of thin airfoils in pitching oscillation. 3rd Report. The range of attack angle where leading edge stall separation occurs during oscillation. [O] . Hiroyuki UENO, Hideo TANAKA, Ichiro FUJIMOTO 1987

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7. Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution With Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58° and Mach Numbers to 2 [R] . Robert L. Kruse, Earl R. Keener, Gary T. Chapman 1979

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Transitional Characteristics of Vortices Issued From A Body Which Creates Asymmetric Flow Field. In A Case of Thin Symmetrical Airfoil With Angle of Attack Under Rotational Oscillation of Small Amplitude.

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