Experimental Study of the Corner Flow Separation on a Simplified Junction
Author:
Affiliation:
1. Applied Aerodynamics Department, ONERA—The French Aerospace Lab, 92190 Meudon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053771
Reference29 articles.
1. A Wing-Body Fairing Design for the DLR-F6 Model: A DPW-III Case Study
2. High-fidelity simulations of unsteady civil aircraft aerodynamics: stakes and perspectives. Application of zonal detached eddy simulation
3. JUNCTION FLOWS
4. An experimental study of a turbulent wing-body junction and wake flow
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