Drag reduction on a bluff body at yaw angles to 30 degrees
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25893
Reference5 articles.
1. ^achmann, G.V. Boundary Layer and Flow Control, Vol.1, Pergamon Press, New York, 1961, pp.463-567.
2. Axisymmetric bluff-body drag reduction through geometrical modification
3. Axisymmetric bluff-body drag reduction using circumferential grooves
4. The Influence of Wind Tunnel Solid Boundaries on Automotive Test Data
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