Analysis of the Chemically Reacting Laminar Boundary Layer during Hybrid Combustion
- 1 December 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (12) , 1691-1698
- https://doi.org/10.2514/3.50671
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Boundary Layer at a Stagnation Point with Hydrogen InjectionCombustion Science and Technology, 1970
- Pressure dependence of nonmetalized hybrid fuel regression rates.AIAA Journal, 1967
- Pressure dependence of hybrid fuel regression rates.AIAA Journal, 1967
- Regression rates of nonmetalized hybrid fuel systemsAIAA Journal, 1965
- Laminar boundary layer with hydrogen injection including multicomponent diffusionAIAA Journal, 1964
- Laminar Boundary - Layer Wedge Flows with Evaporation and CombustionPublished by Elsevier ,1964
- Introductory Considerations on Hybrid Rocket CombustionPublished by Elsevier ,1964
- The Film Combustion of Liquid FuelZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1956