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[American Institute of Aeronautics and Astronautics 21st AIAA Computational Fluid Dynamics Conference - San Diego, CA ()] 21st AIAA Computational Fluid Dynamics Conference - Measurements in Regions of Shock Wave/Turbulent Boundary Layer Interaction from Mach 4 to 10 for Open and “Blind” Code Evaluation/Validation
Holden, Michael S., Wadhams, Tim P., MacLean, Matthew G.Year:
2013
Language:
english
DOI:
10.2514/6.2013-2836
File:
PDF, 5.79 MB
english, 2013