New device for controlling asymmetric flowfields on forebodies at large alpha
Author:
Affiliation:
1. North Carolina State University, Raleigh, North Carolina 27695
2. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46049
Reference14 articles.
1. Effects of nose bluntness, roughness, and surface perturbations on the asymmetric flow past slender bodies at large angles of attack
2. Effects of surface perturbations on the asymmetric vortex flow over a slender body
3. Forebody and missile side forces and the time analogy
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