Validation of code using turbulence model applied to three-dimensional transonic channel
Author:
Affiliation:
1. Societe Nationale d'Etude et de Construction de Moteurs d'Aviation, 77550 Moissy-Cramayel, France
2. ONERA, 92320 Chatillon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12385
Reference18 articles.
1. Viscous-Inviscid Interaction Solvers and Computation of Highly Separated Flows
2. Analytical Theory of Transonic Normal Shock-Turbulent Boundary-Layer Interaction
3. Comparison of Multiequation Turbulence Models for Several Shock Boundary-Layer Interaction Flows
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