Stability Analysis of a Mach 10 Flat-Plate Boundary Layer using a High-Order Non-Equilibrium Solver (AIAA 2018-2084)
Aerospace sciences meeting ; 2018 ; Kissimmee, FL
2018-01-01
18 pages
Conference paper
English
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NON-EQUILIBRIUM EFFECTS ON THE STABILITY OF A MACH 10 FLAT-PLATE BOUNDARY LAYER (AIAA 2017-3162)
British Library Conference Proceedings | 2017
|British Library Conference Proceedings | 2018
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