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
01.01.2018
18 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
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
|