Numerical Investigation of Interaction of Oblique Shock and Detonation Waves in a Steady Supersonic Flow of a Chemical Reactive Gaseous Mixture
RUSSIAN ACADEMY OF SCIENCES NOVOSIBIRSK INST OF THEORETICAL AND APPLIED MECHANICS
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The main objective of the present work is to study the flow structure with reflection of oblique SW and DW in a steady supersonic flow of a chemically reacting mixture and the transition from regular to Mach reflection.
- Fluid Mechanics