Experimental Investigation of Transonic Buffet Control on a Wing Airfoil Using Tangential Jet Blowing
Author:
Publisher
Pleiades Publishing Ltd
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1134/S0015462820040023.pdf
Reference18 articles.
1. L. Bahi, J.M. Ross, and T. Nagamatsu, “Passive shock wave/boundary layer control for transonic airfoil drag reduction,” AIAA Paper 1983–0137 (1983).
2. S. Raghunathan, “Passive control of shock-boundary layer interaction,” Progr. Aerospace Sci.25, 271–296 (1988).
3. J. Birkemeyer, H. Rosemann, and E. Stanewsky, “Shock control on a swept wing,” Aerospace Sci. Technol.4, 147–156 (2000).
4. H. Ogawa, H. Babinsky, M. Patzold, and T. Lutz, “Shock-wave/boundary-layer interaction control using three-dimensional bumps for transonic wings,” AIAA J.46(6), 1442–1452 (2008).
5. H.H. Pearcey, “Shock-induced separation and its prevention by design and boundary layer control,” in: Boundary Layer and Flow Control – Its Principles and Application, Vol. 2, Ed. by Lachmann (Pergamon, London, 1961), pp. 1170–1361.
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