Computation of the poststall behavior of a circulation controlled airfoil
Author:
Affiliation:
1. Sterling Software at NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46647
Reference41 articles.
1. Two-Dimensional Subsonic Wind Tunnel Evaluation of a 20-Percent-Thick Circulation Control Airfoil
2. 2Abramson, J., and Rogers, E. O. "High-Speed Characteristics of Circulation Control Airfoils,'1AIAA Paper 83-0265, Jan. 1983.
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