System Identification of Two-Dimensional Transonic Buffet
Author:
Affiliation:
1. Japan Aerospace Exploration Agency (JAXA), Chofu-shi, Tokyo 182-8522, Japan
2. HESAM University, F-75013 Paris, France
Funder
Japan Society for the Promotion of Science (JSPS), Grants-in-Aid for Scientific Research (KAKENHI) program
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061001
Reference75 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. McDevittJ. B.OkunoA. F. “Static and Dynamic Pressure Measurements on a NACA 0012 Airfoil in the Ames High Reynolds Number Facility,” NASA Ames Research Center TR NASA-TP-2485, 1985.
3. Experimental Study of Shock Oscillation over a Transonic Supercritical Profile
4. Experimental analysis of the shock dynamics on a transonic laminar airfoil
5. Turbulence model and numerical scheme assessment for buffet computations
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