## Internal Combustion Processes of Liquid Rocket Engines: Modeling and Numerical SimulationsThis book concentrates on modeling and numerical simulations of combustion in liquid rocket engines, covering liquid propellant atomization, evaporation of liquid droplets, turbulent flows, turbulent combustion, heat transfer, and combustion instability. It presents some state of the art models and numerical methodologies in this area. The book can be categorized into two parts. Part 1 describes the modeling for each subtopic of the combustion process in the liquid rocket engines. Part 2 presents detailed numerical methodology and several representative applications in simulations of rocket engine combustion. |

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### Contents

Physical Mechanism and Numerical Modeling | |

Engines | |

Atomization | |

References | |

Modeling of Droplet Evaporation and Combustion | |

Modeling of Turbulence | |

Turbulent Combustion Model | |

Heat Transfer Modeling and Simulation | |

The Model of Combustion Instability | |

Liquid Rocket Engines | |

List of Tables | |

### Other editions - View all

Internal Combustion Processes of Liquid Rocket Engines: Modeling and ... Zhen-Guo Wang Limited preview - 2016 |

Internal Combustion Processes of Liquid Rocket Engines: Modeling and ... Zhen-Guo Wang Limited preview - 2016 |

### Common terms and phrases

acoustic AIAA Paper amplitude analysis atomization average boundary conditions calculation centrifugal injector chamber pressure characteristics chemical reaction coaxial coefficient combustion chamber combustion instability combustion process combustion stability combustor component computational concentration constant continuity equation control volume convection cooling denotes discrete distribution disturbance droplet evaporation droplet group droplet surface eddy viscosity equilibrium evaporation model evaporation rate Figure filtered flame flamelet flow field fluctuation fluid frequency fuel gas phase gas–liquid governing equations grid heat conduction heat flux hydrogen images infinitesimal injection interface kerosene large eddy simulation linear liquid jet liquid propellant liquid rocket engine mass method mixture multicomponent nodes nonlinear nozzle numerical simulation obtained oscillation oxidizer oxygen parameters particle premixed flame pressure oscillation probability density function radiation heat transfer reaction rate region scalar solve source term specific heat capacity specific impulse Stefan flow sub-grid tensor thermal thrust chamber transport equation turbulence model unstructured grid vibration mode wave wavelength zone