Effects of Synthetic Jet Actuation on a Ramping NACA 0015 Airfoil
Author:
Affiliation:
1. Texas A&M University, College Station, Texas 77843-3141
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.3500
Reference31 articles.
1. 1Klausmeyer, S. M., Papadakis, M., and Lin, J. C. "A Flow Physics Study of Vortex Generators on a Multi-Element Airfoil," AIAA Paper 96-0548, Jan.1996.
2. Forcing level effects of internal acoustic excitation on the improvement of airfoil performance
3. Separation Control on a Cantilever Wing with a Self-Excited Vibrating Rod
4. 4Tillman, T. G. and Hwang, D. P. "Drag Reduction on a Large-Scale Nacelle Using a Micro-Blowing Technique," AIAA Paper 99-0130, Jan.1999.
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