Shock-Wave/Turbulent Boundary-Layer Interactions in Nonequilibrium Flows
Author:
Affiliation:
1. University of Rome “ La Sapienza,”, 00184 Rome, Italy
2. Centro Italiano Ricerche Aerospaziali, 81043 Capua, Italy
3. ONERA, 92190 Meudon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1209
Reference27 articles.
1. Aerothermodynamic Phenomena and the Design of Atmospheric Hypersonic Airplanes
2. Analysis of hypersonic shock-wave laminar boundary-layer interaction phenomena
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