Numerical simulation of shock-induced combustion/detonation in a premixed H2-air mixture using Navier-Stokes equations
- 24 June 1991
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Multigrid for hypersonic viscous two- and three-dimensional flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- The Structural Stability of Oblique Detonation WavesCombustion Science and Technology, 1990
- Convection of a pattern of vorticity through a reacting shock wavePhysics of Fluids A: Fluid Dynamics, 1990
- Three-dimensional computations of cross-flow injection and combustion in a supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocitiesAIAA Journal, 1988
- A two-dimensional detonation supported by a blunt body or a wedgePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Morphology of a standing oblique detonation wavePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Mechanism of Instabilities of Exothermic Hypersonic Blunt-Body FlowsCombustion Science and Technology, 1971
- A Study of Supersonic CombustionJournal of the Aerospace Sciences, 1960
- A Preliminary Study of the Application of Steady-State Detonative Combustion to a Reaction EngineJournal of Jet Propulsion, 1958