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Prediction of Space and Time Distribution of Wax-based Fuel Regression Rate in a Hybrid Rocket

机译:混合火箭中蜡基燃料回归率的空间和时间分布的预测

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A numerical set up has been developed to predict the axial distribution and time history of fuel regression rates with the aim of comparing numerical results with the experimental data. The numerical approach is based on a quasi-one-dimensional CFD strategy, which is coupled with chemical equilibrium combustion; the wax-fuel regression rate has been simulated with the liquefying fuel theory developed by Karabeyoglu. In this model, local radiation heat transfer from both the hot gas combustion molecules (CO, CO_2, and H_2O) and soot particles is considered. It is shown that, when radiation heating of the fuel is taken into account, the calculated fuel regression rates exhibit values and axial profiles close to the ones observed experimentally.
机译:已经开发了一种数值设置,以预测燃料回归速率的轴向分布和时间历史,目的是将数值结果与实验数据进行比较。数值方法基于准一维CFD策略,与化学平衡燃烧相结合;通过Karabeyoglu开发的液化燃料理论模拟了蜡燃料回归率。在该模型中,考虑来自热气体燃烧分子(CO,CO_2和H_2O)和烟灰颗粒的局部辐射热传递。结果表明,当考虑燃料的辐射加热时,计算出的燃料回归速率表现出靠近实验观察到的值和轴向曲线。

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