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Prediction Method of Unsteady Combustion Around Hypersonic Projectile in Stoichiometric...
- Source :
-
AIAA Journal . Oct98, Vol. 36 Issue 10, p1834. 8p. - Publication Year :
- 1998
-
Abstract
- Proposes an effective nondimensional parameter, referred to as the first Damkohler parameter, to quantitatively classify the unsteady flow regime of shock-induced combustion around a hypervelocity spherical projectile. Development of a prediction method; Computational study for validation; Results of the study.
- Subjects :
- *PREDICTION theory
*HYPERSONIC aerodynamics
COMBUSTION measurement
Subjects
Details
- Language :
- English
- ISSN :
- 00011452
- Volume :
- 36
- Issue :
- 10
- Database :
- Academic Search Index
- Journal :
- AIAA Journal
- Publication Type :
- Academic Journal
- Accession number :
- 1168215
- Full Text :
- https://doi.org/10.2514/2.299