Large-Eddy Simulation of Shock/Boundary-Layer Interaction
Author:
Affiliation:
1. Institut National des Sciences Appliquées de Rouen, 76801 Saint Etienne du Rouvray, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051786
Reference58 articles.
1. Wall Pressure Fluctuations in an Over-Expanded Rocket Nozzle
2. Girard, S. "Etude des Charges Latérales dans une tuyère Supersonique Surdétendue," Ph.D. Thesis,University of Poitiers, Poitiers, France, 1999.
3. Laser Doppler velocimeter measurements in unsteady, separated, transonic diffuser flows
4. Forced oscillation experiments in supercritical diffuser flows
5. Wall Pressure Fluctuations in a Turbulent Boundary Layer over a Bump
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