Drag reduction in transonic shock-wave/boundary-layer interaction using porous medium: a computational study
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Physics and Astronomy,Mechanical Engineering
Link
https://link.springer.com/content/pdf/10.1007/s00193-021-01009-7.pdf
Reference63 articles.
1. Stanewsky, E., Délery, J., Fulker, J., Geißler, W. (eds.): EUROSHOCK—Drag Reduction by Passive Shock Control, Results of the Project EUROSHOCK, AER2-CT92-0049 Supported by the European Union, 1993–1995, Notes on Numerical Fluid Mechanics, vol. 56. Vieweg-Teubner Verlag, Wiesbaden (1997). https://doi.org/10.1007/978-3-322-90711-0
2. Stanewsky, E., Délery, J., Fulker, J., Matteis, P. (eds.): Drag Reduction by Shock and Boundary Layer Control, Results of the Project EUROSHOCK II, Supported by the European Union 1996–1999, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol. 80. Springer, Berlin (2002). https://doi.org/10.1007/978-3-540-45856-2
3. Bahi, L., Ross, J., Nagamatsu, H.: Passive shock wave/boundary layer control for transonic airfoil drag reduction. 21st Aerospace Sciences Meeting, Reno, NV, AIAA Paper 1983-0137 (1983). https://doi.org/10.2514/6.1983-137
4. McCormick, D.C.: Shock/boundary-layer interaction control with vortex generators and passive cavity. AIAA J. 31(1), 91–96 (1993). https://doi.org/10.2514/3.11323
5. Bur, R., Corbel, B., Délery, J.: Study of passive control in a transonic shock wave/boundary-layer interaction. AIAA J. 36(3), 394–400 (1998). https://doi.org/10.2514/2.376
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