Steady State Characteristics of Scramjet Engines Using Hydrogen for High Mach Numbers (AIAA 2017-2294)
AIAA Interantional Space Planes and Hypersonic Systems and Technologies (Conference)
2017-01-01
10 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2014
|COUPLED CONJUGATE HEAT TRANSFER SIMULATION FOR A SCRAMJET INLET AT MACH 8 (AIAA 2017-4502)
British Library Conference Proceedings | 2017
|DataCite | 1889
Target-Edge Based Orthogonal Anisotropic Mesh (AIAA 2015-2294)
British Library Conference Proceedings | 2015
|