Wake Vortex Measurements of an Ogive Cylinder at CY = 36 Degrees
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference10 articles.
1. The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidence
2. Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack
3. Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream
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1. Aerodynamic forces and moments on an ogive cylinder at incidence;The Aeronautical Journal;2004-06
2. Effects of Probe Interference on Side Force of an Inclined Ogive Cylinder;AIAA Journal;2004-02
3. Compressible flow past a contour and stationary vortices;Journal of Fluid Mechanics;1987-05
4. Asymmetric flowfield development on a slender body at high incidence;AIAA Journal;1984-02
5. Multistable vortex patterns on slender, circular bodies at high incidence;AIAA Journal;1982-04
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