Numerical Simulation of the Evolution of Turbulent Spots in a Supersonic Boundary Layer over a Plate
Author:
Publisher
Pleiades Publishing Ltd
Subject
Computational Mathematics,Modeling and Simulation
Link
https://link.springer.com/content/pdf/10.1134/S2070048223010076.pdf
Reference14 articles.
1. R. Narasimha, “The laminar-turbulent transition zone in the boundary layer,” Prog. Aerosp. Sci. 22 (1), 29–80 (1985). https://doi.org/10.1016/0376-0421(85)90004-1
2. J. P. Clark, T. V. Jones, and J. E. LaGraff, “On the propagation of naturally-occurring turbulent spots,” J. Eng. Math. 28 (1), 1–19 (1994). https://doi.org/10.1007/BF02383602
3. D. J. Mee and C. P. Goyne, “Turbulent spots in boundary layers in a free-piston shock-tunnel flow,” Shock Waves 6 (6), 337–343 (1996). https://doi.org/10.1007/BF02511324
4. D. J. Mee, “Boundary-layer transition measurements in hypervelocity flows in a shock tunnel,” AIAA J. 40 (8), 1542–1548 (2002). https://doi.org/10.2514/2.1851
5. L. Krishnan and N. D. Sandham, “Effect of Mach number on the structure of turbulent spots,” J. Fluid Mech. 566, 225–234 (2006), https://doi.org/10.1017/S0022112006002412
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