The study concerns gas-wave-dynamic phenomena during the transient state from combustion initiation to stable detonation. The results should provide basic information on the generation of pressure waves by explosive reactions, important to understanding of combustion instability in rocket chambers and similar devices, as, for instance, supersonic combustion propulsion systems for hypersonic flight vehicles. (Author)
Study of the Development and Stabilization of Detonations
1966
10 pages
Report
No indication
English
A study of heterogeneous detonations
AIAA | 1966
|AIAA | 2006
|Shock induced heterogeneous detonations.
NTRS | 1965
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