Measurements of lateral aerodynamics characteristics of forebodies at high angle of attack in subsonic and transonic flows
Author:
Affiliation:
1. Technion - Israel Institute of Technology, Haifa
2. Rafael Armament Development Authority, Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-174
Reference18 articles.
1. Euler solution of axisymmetric flows about bodies of revolution using a multigrid method
2. Zilliak, G.G. "A computational / experimental study of the vortical flow field on a body of revolution at angle of attack". AIAA Paper 87-2277-CP, August 1987.
3. Sreekanth, A.K. and Panneerselvam, S. "Symmetric separated flowpast slender bodies at anglesof attack in subsonic andsupersonic flows", AIAA Paper 85-5007,October 1985.
4. Calculation of symmetric vortex separation affecting subsonic bodiesat high incidence
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