Numerical analysis of reactive turbulent flow in the thrust chamber of RD-108 engine rocket
| Autor: | Seyed Reza Taghavi, Mohammad Ali Dehnavi, Ali Ghafouri |
|---|---|
| Jazyk: | angličtina |
| Rok vydání: | 2019 |
| Předmět: |
Propellant
Kerosene business.industry Turbulence Mechanical Engineering Metals and Alloys Computational Mechanics Thrust Mechanics Impulse (physics) Computational fluid dynamics Physics::Fluid Dynamics Military Science Ceramics and Composites Combustion chamber Liquid oxygen Physics::Chemical Physics business |
| Zdroj: | Defence Technology, Vol 15, Iss 4, Pp 565-575 (2019) |
| ISSN: | 2214-9147 |
| Popis: | Combustion chamber modeling and simulation of the liquid propellant engine with kerosene as fuel and liquid oxygen as an oxidizer in the turbulent flow field are performed by CFD technique. The flow is modeled as Single-phase in steady state and using RNG k-ɛ turbulence model. Simulation results are validated by experimental data of thrust, special impulse and combustion chamber pressure. By comparing two reaction models of finite rate chemistry and frozen model with experimental data, it is concluded that finite rate chemistry has acceptable results. The optimum value of equivalence ratio (oxidizer to fuel ratio) per reaction and operational parameters of the engine which maximize thrust and special impulse are determined. Keywords: Liquid propellant engine, Computational fluid dynamics (CFD), Kerosene and oxygen, Freeze model, Finite rate chemistry model |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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