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Stabilization of detonation combustion of hydrogen-oxygen mixture in a supersonic nozzle.
| Content Provider | CiteSeerX |
|---|---|
| Author | Shatalov, O. P. |
| Abstract | It is considered ignition and combustion of stoichiometric hydrogen-oxygen mixtures diluted by argon inside axisymmetric supersonic nozzle. Incoming into the nozzle flow is supposed to be supersonic and uniform one. A reality of stabilization of detonation combustion of these hydrogen-oxygen mixtures is numerically studied at different values of incoming flow Mach number. Investigations are fulfilled on the base of Euler’s 2D gas dynamics equations for a multi-component mixture. Detailed model of chemical transformations is used. Obtained propulsive force is compared with a resistance force of a conic capsule containing a considered nozzle. |
| File Format | |
| Access Restriction | Open |
| Subject Keyword | Detonation Combustion Hydrogen-oxygen Mixture Supersonic Nozzle Axisymmetric Supersonic Nozzle Conic Capsule Chemical Transformation Flow Mach Number Different Value Gas Dynamic Equation Stoichiometric Hydrogen-oxygen Mixture Propulsive Force Multi-component Mixture Nozzle Flow Detailed Model Resistance Force Uniform One |
| Content Type | Text |