Pressure dependence of nonmetalized hybrid fuel regression rates.
- 1 April 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (4) , 774-778
- https://doi.org/10.2514/3.4061
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Comment on "Choked Flow: A Generalization of the Concept and Some Experimental Data''AIAA Journal, 1966
- Errata: "Theory of Electrostatic Double Probe Comprised of Two Parallel Plates"AIAA Journal, 1966
- Nonequilibrium anomalies in the development of diffusion flames.AIAA Journal, 1966
- Hybrid rocket combustion regression rate model.AIAA Journal, 1966
- Regression rates of nonmetalized hybrid fuel systemsAIAA Journal, 1965
- Ignition and extinction in combustion of initially unmixed reactantsJournal of Fluid Mechanics, 1965
- The structure of the zone of diffusion controlled reactionChemical Engineering Science, 1963
- TURBULENT BOUNDARY LAYER COMBUSTION IN THE HYBRID ROCKETPublished by Elsevier ,1963
- Letter to the editorCombustion and Flame, 1961
- The Film Combustion of Liquid FuelZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1956