A multicomponent boundary layer chemically coupled to an ablating surface.
- 1 June 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (6), 1063-1071
- https://doi.org/10.2514/3.4138
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Sublimation of graphite at hypersonic speedsAIAA Journal, 1965
- Simulation of rocket-nozzle environments with an arc-plasma generatorAIAA Journal, 1965
- Laminar boundary layer with hydrogen injection including multicomponent diffusionAIAA Journal, 1964
- Nonequilibrium, nonsimilar solutions of the laminar boundary-layer equationsAIAA Journal, 1964
- Technical NotesJournal of Jet Propulsion, 1957