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Detailed mechanism of the unsteady combustion around hypersonic projectiles.
- Source :
-
AIAA Journal . Oct96, Vol. 34 Issue 10, p2082. 8p. 2 Black and White Photographs, 8 Diagrams, 1 Chart, 8 Graphs. - Publication Year :
- 1996
-
Abstract
- Studies the flow features of an unsteady shock-induced combustion around projectiles using a series of simulations of an oxygen-hydrogen reaction mechanism. Mechanism of the unsteady combustion around hypersonic projectiles; Characterization of the combustion; Mechanism of the wave interaction on the stagnation streamline; Mechanisms for the large-disturbance regime.
- Subjects :
- *COMBUSTION
*PROJECTILES
Subjects
Details
- Language :
- English
- ISSN :
- 00011452
- Volume :
- 34
- Issue :
- 10
- Database :
- Academic Search Index
- Journal :
- AIAA Journal
- Publication Type :
- Academic Journal
- Accession number :
- 9711240035
- Full Text :
- https://doi.org/10.2514/3.13355