Asymmetric Vortex Wake Development on Missiles at High Angles of Attack
Author:
Affiliation:
1. TRW Defense and Space Systems Group, Redondo Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.57174
Reference13 articles.
1. Jorgensen, L. H. and Nelson, E. R. "Experimental Aerodynamic Characteristics for a Cylindrical Body of Revolution with Various Noses at Angles of Attack from 0° to 58° and Mach Numbers from 0.6to 2.0,"NASATMX-3128, Dec. 1974.
2. Side Forces on Ogive-Cylinder Bodies at High Angles of Attack in Transonic Flow
3. Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack
4. Body vortex formation on missiles at high angles of attack
5. Aerodynamic forces and moments on a slender body with a jet plume for angles of attack up to 180 degrees
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