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Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet
Aerospace Science and Technology ( IF 5.0 ) Pub Date : 2024-06-25 , DOI: 10.1016/j.ast.2024.109357 Jincheng Zhang , Zhenguo Wang , Chaoyang Liu , Mingbo Sun , Hongbo Wang , Junding Ai , Zihao Zhang
Aerospace Science and Technology ( IF 5.0 ) Pub Date : 2024-06-25 , DOI: 10.1016/j.ast.2024.109357 Jincheng Zhang , Zhenguo Wang , Chaoyang Liu , Mingbo Sun , Hongbo Wang , Junding Ai , Zihao Zhang
As the Mach number increases, the local static temperature gradually approaches the characteristic gas vibration/dissociation temperature, and significant thermo-chemical relaxation processes occur. The thermo-chemical nonequilibrium phenomenona could affect the mixing and combustion process and become a factor that must be considered for scramjet design. In this paper, a large eddy simulation solver based on the two-temperature model is developed. The transfer terms between vibrational and trans-rotational energy are modeled by the Landau–Teller formulation and the vibrational-dissociation coupling is considered by adopting the Park model. Three sets of simulations based on the Hyshot Ⅱ engine configuration with different models were performed simultaneously to validate numerical methods and analyze results. The results reveal that the shock, cross-injection of fuel, and Prandtl-Meyer flow induce significant nonequilibrium regions. The vibration relaxation process in the jet mixing region is frozen, the vibration temperature is much higher than the trans-rotational temperature, and the extra energy is converted from the vibration mode to the trans-rotational mode, resulting in the increase of the trans-rotational temperature and the advance of auto-ignition in the nonequilibrium condition. Considering the vibration-dissociation coupling, the higher vibration temperature promotes dissociation. It inhibits the generation of active radicals in the ignition process, weakening the enhancement effect of nonequilibrium on auto-ignition. In the expanded nozzle, the concentrations of molecules and trans-rotational temperature in nonequilibrium cases are slightly lower than those in the equilibrium case due to the enhancement of dissociation.
中文翻译:
热化学非平衡对超燃冲压发动机横向射流燃烧特性的影响
随着马赫数的增加,局部静态温度逐渐接近特征气体振动/离解温度,并发生显着的热化学弛豫过程。热化学非平衡现象会影响混合和燃烧过程,成为超燃冲压发动机设计必须考虑的因素。本文开发了一种基于二温模型的大涡模拟求解器。振动能量和跨旋转能量之间的传递项采用 Landau-Teller 公式建模,并采用 Park 模型考虑振动-解离耦合。基于Hyshot Ⅱ发动机配置不同型号的三组模拟同时进行,以验证数值方法并分析结果。结果表明,激波、燃料交叉喷射和普朗特-迈耶流会产生显着的非平衡区域。射流混合区的振动弛豫过程被冻结,振动温度远高于跨转温度,多余的能量从振动模式转换为跨转模式,导致跨转温度升高。旋转温度和非平衡条件下自燃的提前。考虑到振动-解离耦合,较高的振动温度会促进解离。它抑制着火过程中活性自由基的产生,减弱非平衡对自燃的增强作用。在膨胀喷嘴中,由于解离的增强,非平衡情况下的分子浓度和转转温度略低于平衡情况。
更新日期:2024-06-25
中文翻译:
热化学非平衡对超燃冲压发动机横向射流燃烧特性的影响
随着马赫数的增加,局部静态温度逐渐接近特征气体振动/离解温度,并发生显着的热化学弛豫过程。热化学非平衡现象会影响混合和燃烧过程,成为超燃冲压发动机设计必须考虑的因素。本文开发了一种基于二温模型的大涡模拟求解器。振动能量和跨旋转能量之间的传递项采用 Landau-Teller 公式建模,并采用 Park 模型考虑振动-解离耦合。基于Hyshot Ⅱ发动机配置不同型号的三组模拟同时进行,以验证数值方法并分析结果。结果表明,激波、燃料交叉喷射和普朗特-迈耶流会产生显着的非平衡区域。射流混合区的振动弛豫过程被冻结,振动温度远高于跨转温度,多余的能量从振动模式转换为跨转模式,导致跨转温度升高。旋转温度和非平衡条件下自燃的提前。考虑到振动-解离耦合,较高的振动温度会促进解离。它抑制着火过程中活性自由基的产生,减弱非平衡对自燃的增强作用。在膨胀喷嘴中,由于解离的增强,非平衡情况下的分子浓度和转转温度略低于平衡情况。