Approach to side force alleviation through modification of the pointed forebody geometry
Author:
Affiliation:
1. University of British Columbia, Vancouver, British Columbia, V6T1Z4 Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46135
Reference22 articles.
1. Aerodynamics of pointed forebodies at high angles of attack
2. Vortex-induced asymmetric loads in 2-D and 3-D flows
3. Alleviation of Vortex-Induced Asymmetric Loads
4. Maximum vortex-induced side force revisited
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. Dynamic responses of asymmetric vortices over slender bodies to a rotating tip perturbation;Experiments in Fluids;2016-03-30
2. Asymmetric Flow Around High-Angle-of-Attack Slender Bodies;Fluid Dynamics of High Angle of Attack;1993
3. High Angle of Attack Missile Aerodynamics;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;1993-01
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