Laminar-turbulent transition in supersonic boundary layers with surface heat transfer: A numerical study
Author:
Affiliation:
1. CNRS-University and INSA of Rouen, Normandie University, CORIA-UMR 6614, Rouen, France
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
https://www.tandfonline.com/doi/pdf/10.1080/10407782.2017.1353380
Reference34 articles.
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5. D. J. Bodony, Instability and Transition of a Mach-5.8 at Plate Boundary Layer Over a Thermo-Mechanically Compliant Panel, Proceedings of the Summer Program, Center for Turbulence Research, pp. 185–192, 2016.
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