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首页> 外文期刊>Journal de Physique, IV: Proceedings of International Conference >Numerical modeling and simulation of RAMAC 30 experiment carried out at the French-German research institute of Saint-Louis
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Numerical modeling and simulation of RAMAC 30 experiment carried out at the French-German research institute of Saint-Louis

机译:法国-圣路易斯研究所的RAMAC 30实验的数值建模和仿真

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摘要

A ram accelerator experiment which was done in ISL's RAMAC 30, was numerically simulated in this study. The case of shot 225 was considered and the initial projectile launching speed was 1.8 km/s which corresponded to the superdetonative speed of the stoichiometric H_2/O_2 mixture diluted with 5CO_2. CFD code had some enhanced features suitable for the high-pressure gaseous combustion. In this study, it was found that neither shock heating nor viscous heating was sufficient to ignite the mixture at the low speed of 1.8 km/s, as was found in the experiments using a steel-covered projectile. However, we could succeed in igniting the mixtures by imposing an amount of additional heat to the combustor section and simulate the positive acceleration of the shot 225 with an aluminum-covered projectile in reasonable agreement. Some additional studies were preformed concerning the location of the forced ignition and the conical angle of the projectile. The results gave some insights into the combustion mechanism and the condition of positive acceleration in a scram accelerator.
机译:在这项研究中,对在ISL的RAMAC 30中完成的ram加速器实验进行了数值模拟。考虑了225炮的情况,初始弹丸发射速度为1.8 km / s,对应于用5CO_2稀释的化学计量的H_2 / O_2混合物的超爆速度。 CFD代码具有一些适用于高压气体燃烧的增强功能。在这项研究中,发现在以1.8 km / s的低速行驶时,冲击加热和粘性加热都不足以点燃混合物,这是在使用钢制覆盖弹丸的实验中发现的。但是,我们可以通过向燃烧室施加一定量的额外热量来成功点燃混合物,并以合理的协议模拟铝覆盖弹丸对子弹225的正加速度。关于强制点火的位置和弹丸的圆锥角,还进行了一些其他研究。结果为燃煤加速器的燃烧机理和正加速条件提供了一些见识。

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