Quasi-CJ rotating detonation with partially premixed methane-oxygen injection: Numerical simulation and experimental validation

Pierre Hellard , Thomas Gaillard , Dmitry Davidenko , Patrick Berterretche , Ratiba Zitoun , Pierre Vidal
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Abstract

The efficiency gain of rotating detonation depends on several loss factors related to the chamber geometry, the injection principle, the propellants and their mass flow rates, and the equivalence ratio. Numerical simulation can help quantify these losses, and this work presents a Large Eddy Simulation (LES) of rotating detonation in an annular chamber and its validation against experiments. The simulation captured the mixing processes, the overall dynamics of the detonation, the deflagration, and the burnt gas expansion. The injection device was numerically designed to ensure partial premixing of the propellants before injection into the chamber. The chamber had a length of 110 mm, an outer diameter of 80 mm, and a radial width of 10 mm. The mixture consisted of gaseous CH4 and O2 with an equivalence ratio of 1.2 and a mass flow rate of 160 g/s. Combustion kinetics was modeled using a skeletal mechanism with 62 reactions and 16 species. The boundary conditions were adiabatic slip walls. The results reproduce well the detonation velocity (within 1% deviation) and the pressure variation behind the wave. The simulated OH* chemiluminescence compares well with experimental high-speed imaging of the outlet and side of the chamber. The simulation results indicate that 65% of the propellant mass is well mixed in front of the wave whereas 15% of the mixture is burned by deflagration. They show that CH4 and O2 do not axially stratify because they have similar injection dynamics between periodic perturbations induced by the rotating detonation. Good propellant mixing and low deflagration losses explain the high experimental detonation velocity, about 90% of DCJ, and a high combustion efficiency of 98%. These agreements between the computational and experimental results indicate that the simulation is capable of capturing the physical scales relevant to RDC operation and producing reliable results for RDC design.

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部分预混甲烷-氧气喷射的准 CJ 旋转爆轰:数值模拟和实验验证
旋转爆轰的效率增益取决于与爆轰室几何形状、喷射原理、推进剂及其质量流量以及等效比相关的几个损耗因素。数值模拟有助于量化这些损失,本研究介绍了环形腔中旋转起爆的大涡流模拟(LES)及其与实验的验证。模拟捕捉了混合过程、爆轰的整体动态、爆燃和燃烧气体膨胀。对喷射装置进行了数值设计,以确保在将推进剂喷入燃烧室之前进行部分预混合。推进室长度为 110 毫米,外径为 80 毫米,径向宽度为 10 毫米。混合物由气态 CH4 和 O2 组成,当量比为 1.2,质量流量为 160 克/秒。燃烧动力学模型采用骨架机理,包括 62 个反应和 16 个物种。边界条件为绝热滑壁。结果很好地再现了爆炸速度(偏差在 1%以内)和波后压力变化。模拟的 OH* 化学发光与试验室出口和侧面的高速成像对比良好。模拟结果表明,65% 的推进剂在波前充分混合,而 15%的混合物则爆燃燃烧。模拟结果表明,CH4 和 O2 不会发生轴向分层,因为它们在旋转爆燃引起的周期性扰动之间具有相似的喷射动态。良好的推进剂混合和较低的爆燃损失解释了为什么实验中的爆燃速度很高,约为 DCJ 的 90%,而且燃烧效率高达 98%。计算和实验结果之间的这些一致性表明,模拟能够捕捉到与 RDC 运行相关的物理尺度,并为 RDC 设计提供可靠的结果。
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