Experimental Investigation of Mach Number and Pressure Gradient Effects on Boundary Layer Transition in Two-Dimensional Flow
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Springer International Publishing
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http://link.springer.com/content/pdf/10.1007/978-3-319-64519-3_28
Reference15 articles.
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3. Costantini, M., Risius, S., Klein, C: Experimental investigation of the effect of forward-facing steps on boundary layer transition. In: Medeiros, M.A.F., Meneghini, J.R. (eds.) IUTAM_ABCM Symposium on Laminar Turbulent Transition, Procedia IUTAM, Vol. 14, pp. 152–162 (2015)
4. Costantini, M., Hein, S., Henne, U., Klein, C., Koch, S., Schojda, L., Ondrus, V., Schröder, W.: Pressure gradient and nonadiabatic surface effects on boundary layer transition. AIAA J. 54(11), 3465–3480 (2016)
5. Costantini, M., Risius, S., Klein, C: Effect of forward-facing steps on boundary layer transition at a subsonic Mach Number. In: Dillmann, A., Heller, G., Krämer, E., Wagner, C., Breitsamter, C. (eds.) New Results in Numerical and Experimental Fluid Mechanics X, Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), Vol. 132, pp. 203–213. Springer, Berlin/Heidelberg (2016)
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