Performance and Energy Expenditure of Coflow Jet Airfoil with Variation of Mach Number
Author:
Affiliation:
1. University of Miami, Coral Gables, Florida 33124
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033113
Reference34 articles.
1. Circulation Control for High Lift and Drag Generation on STOL Aircraft
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4. EnglarR. J. “Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modifications; Past, Present and Future,” AIAA Paper 2000-2541, 2000.
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