Laminar-to-turbulent transition in supersonic boundary layer: Effects of initial perturbation and wall heat transfer
Author:
Affiliation:
1. CORIA-UMR 6614, CNRS-University, INSA of Rouen and Normandie University, Rouen, France
Funder
Grand Equipement National de Calcul Intensif
Publisher
Informa UK Limited
Subject
Condensed Matter Physics,Numerical Analysis
Link
https://www.tandfonline.com/doi/pdf/10.1080/10407782.2018.1464785
Reference31 articles.
1. Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature
2. The Computational Modeling of Transitional Flow through a Transonic Linear Turbine: Comparative Performance of Various Turbulence Models
3. Heat Transfer in Turbulent Boundary Layers of Conical and Bell Shaped Rocket Nozzles with Complex Wall Temperature
4. Transition Experiments on Blunt Bodies with Isolated Roughness Elements in Hypersonic Flight
5. Laminar Boundary-Layer Oscillations and Stability of Laminar Flow
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