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NUMERICAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF TWO DIFFERENT COMPONENT BODIES AT VARIOUS ANGLES OF ATTACK

机译：两种不同部件在各种攻击角度的空气动力学特征的数值研究

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N.P. Skibina; N.R. Gimaeva; N.V. Savkina; E.A. Maslov;
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1. Experimental Investigation of Aerodynamic Characteristics on Slender Bodies at High Angles of Attack [J] . Peiqing Liu, Xueying Deng Canadian Aeronautics and Space Journal . 2003,第1期

机译：大迎角细长体气动特性的实验研究
2. Experimental Investigation of Aerodynamic Characteristics on Slender Bodies at High Angles of Attack [J] . Peiqing Liu, Xueying Deng Canadian Aeronautics and Space Journal . 2003,第1期

机译：大迎角细长体气动特性的实验研究
3. Unsteady aerodynamic characteristics of slender body at extra-wide angle-of-attack range [J] . Wang Fangjian, Liu Jin, Qin Han, Aerospace science and technology . 2021,第Mara期

机译：在超广角攻角范围内纤细体积的不稳定空气动力学特性
4. NUMERICAL INVESTIGATIONS ON THE SLENDER AXISYMMETRIC BODIES AERODYNAMICS IN WIDE RANGE OF MACH NUMBERS AND ANGLES OF ATTACK FROM 0° TO 180° [C] . N.V. Voevodenko, L.G. Ivanteeva, V.Ju. Lunin Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：0°至180°范围内马赫数和攻角宽范围内的轴对称机构气动的数值研究
5. Aerodynamic control of slender bodies from low to high angles of attack through flow manipulation. [D] . Lopera, Javier. 2007

机译：通过流动操纵，从低到高攻角对细长体进行气动控制。
6. Numerical Investigation of Aerodynamic Noise Reduction of Nonpneumatic Tire Using Nonsmooth Riblet Surface [O] . Haichao Zhou, Zhen Jiang, Jian Yang, 2020

机译：用非光滑的Riblet表面降低非充气轮胎气动噪声的数值研究
7. Numerical Investigation of Crossflow Separation on a Tangent-Ogive Forebody at High Angle of Attack. [O] . Shing-Chung ONN, Nai-Chung YANG, Jih-Lan HSIUNG, 1997

机译：高迎角切线型前体跨流分离的数值研究。
8. 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

机译：旋转圆柱体的非对称气动特性研究，其中鼻子几何形状的变化和攻角为58°，马赫数为2的旋转方向

NUMERICAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF TWO DIFFERENT COMPONENT BODIES AT VARIOUS ANGLES OF ATTACK

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