Numerical Investigation of Flow Asymmetry Around Slender Body at High Angles of Attack-Reference-Cited by-同舟云学术

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Numerical Investigation of Flow Asymmetry Around Slender Body at High Angles of Attack

Published:2016-01-02 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA Aerospace Sciences Meeting
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Author:

AlQadi Ibraheem M.¹,Eljack Elteyeb¹

Affiliation:

1. King Abdulaziz University

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. Asymmetric Vortices on a Slender Body of Revolution

2. 2Gowen, F. E. and Perkins, E. W. “A Study of the Effects of Body Shape on the Vortex Wakes of Inclined Bodies at a Mach Number of 2,” Tech. Rep. NACA-RM-A53I17, NACA, 1953.

3. Induced side forces at high angles of attack

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Influence of Roughness on the Asymmetric Flow Field of a Slender Body;International Journal of Aerospace Engineering;2022-07-27

2. Investigation of asymmetric flow past a slender body at high angles of attack;Theoretical and Computational Fluid Dynamics;2019-08-27

3. Computational Study of Asymmetric Wake-Vortex Around Ogive-Cylinder Body at High Angles of Attack;2018 AIAA Aerospace Sciences Meeting;2018-01-07

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