An Investigation of a Slender Forebody Maneuvering at Incidence in High Reynolds Number Flow
Author:
Affiliation:
1. Aeroprobe Corporation
2. Virginia Polytechnic Institute and State University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-669
Reference24 articles.
1. Forebody vortex control - A progress review
2. Panzer, E. C., Rediniotis,O. K. and Telionis, D.P."TheHemisphere-Cylinder inDynamicPitch-Up Motions," AIAA Paper No. 93-2963.
3. Ying, S.X. , Steger, J.L. , Schiff, L.B. and Baganoff, D. , Numerical Simulation of Unsteady, Viscous, High - Angle-of- Attack Flows Usinga PartiallyFlux-Split Algorithm, AIAA Paper 86 -2179, June1986.
4. The scaling and control of vortex geometry behind pitching cylinders
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1. Recent progress on the study of asymmetric vortex flow over slender bodies;Acta Mechanica Sinica;2008-09-26
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