Effect of Finite Chemical Reaction Rates on Heat Transfer to the Walls of Combustion-Driven Supersonic MHD Generator Channels
- 1 March 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (3) , 403-404
- https://doi.org/10.2514/3.49252
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental dataAIAA Journal, 1970
- The turbulence structure of equilibrium boundary layersJournal of Fluid Mechanics, 1967