| Autor: |
Xue Li Xia, De Song Liu, Hong Fu Qiang, Guang Wang |
| Rok vydání: |
2012 |
| Předmět: |
|
| Zdroj: |
Advanced Materials Research. :1334-1338 |
| ISSN: |
1662-8985 |
| DOI: |
10.4028/www.scientific.net/amr.452-453.1334 |
| Popis: |
The numerical simulation, based on computational fluid dynamics methodology, has been performed to study the two-phase turbulent combustion flow in rocket engine using non-metallized multicomponent propellant. A reduced reaction mechanism is developed for modelling combustion of fuel droplets in the absence of metal. Gas governing equations are two dimensional axisymmetric N-S equations in Eulerian coordinates. The trajectory model is adopted to analyse the droplet-phase including the droplet collision, breakup and evaporation. The gas flow is influenced by the droplets by adding source term to N-S equations. The reliability of the simulation programme is validated by comparing numerical simulation result with engine test data. |
| Databáze: |
OpenAIRE |
| Externí odkaz: |
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