High-Fidelity Simulations of Afterbody Vortex Flows
Author:
Affiliation:
1. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058284
Reference37 articles.
1. Interference-free measurements of the subsonic aerodynamics of slanted-base ogive cylinders
2. Experimental investigation of the flowfield about an unswept afterbody
3. Reduction of Fuselage Form Drag by Vortex Flows
4. CalareseW.CrislerW. P.GustafsonG. L. “Afterbody Drag Reduction by Vortex Generators,” AIAA Paper 1985-0354, Jan. 1985. doi:10.2514/6.1985-354
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