Investigation of vortex patterns on slender bodies at high angles ofattack
Author:
Affiliation:
1. Nanjing Aeronautical Institute, Nanjing, China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45306
Reference13 articles.
1. Vortex-induced asymmetric loads in 2-D and 3-D flows
2. The flow field about and forces on slender bodies at high angles of attack
3. The effect of roll angle on the flow over a slender body of revolution at high angles of attack
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1. Aerodynamic forces and moments on an ogive cylinder at incidence;The Aeronautical Journal;2004-06
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