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基于特征时间模型的高效喷雾燃烧数值模拟
引用本文:尹钰,杨天威,周华,任祝寅,林宏军,尚守堂.基于特征时间模型的高效喷雾燃烧数值模拟[J].航空动力学报,2023,38(1):104-115.
作者姓名:尹钰  杨天威  周华  任祝寅  林宏军  尚守堂
作者单位:1.清华大学 航天航空学院,北京 100084
基金项目:国家自然科学基金(91841302);国家科技重大专项(2017- Ⅰ -0004-0005)
摘    要:开展了基于特征时间(CTS)燃烧模型的高效喷雾燃烧数值模拟研究。基于CTS模型与层流有限速率燃烧模型对CFM56航空发动机模型燃烧室进行了两相数值模拟,通过比较预测的火焰结构验证了CTS燃烧模型在喷雾燃烧中的适用性。通过采用CTS模型初始化燃烧场来提高有限速率燃烧模型的数值模拟效率,提出了基于CTS燃烧模型结合降维方法的高效数值模拟方法。结果表明:CTS燃烧模型较好预测了CFM56模型燃烧室的火焰形态和组分分布,可为有限速率燃烧模型的数值模拟提供良好的初始解;采用自适应建表(ISAT)方法可减小计算时间90%,在此基础上,基于CTS模型初始化的稳态算例收敛时间减少35%,进一步结合降维方法收敛时间减少40%,证明了CTS模型具有提高喷雾燃烧数值模拟效率的潜力。

关 键 词:特征时间燃烧模型  有限速率燃烧模型  喷雾燃烧  燃烧室  高效算法
收稿时间:2021-07-12

Efficient spray combustion simulations using the characteristic timescale model
Institution:1.School of Aerospace Engineering,Tsinghua University,Beijing 100084,China2.Institute for Aero Engine,Tsinghua University,Beijing 100084,China3.Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang 110015,China
Abstract:The characteristic time scale (CTS) model was investigated for efficient and robust spray combustion simulations. This model was demonstrated in steady-state simulations of spray flames in an aero-engine model combustor, and the predicted temperature and species results were compared with those from the finite-rate combustion model to verify the feasibility of the CTS model in spray combustion. Combined with a dimension reduction method, the CTS model can be used to facilitate the finite-rate based calculations with full chemical kinetics by providing good initial conditions. The accelerating effect was investigated. Results showed that for the CFM56 model combustor considered, CTS yielded a realistic flame shape and reasonably predicted species distributions. The in situ adaptive tabulation (ISAT) approach reduced the calculation time by 90%. The convergence time of steady-state simulations with initialization based on the CTS model was reduced by 35% and then reduced by 40% if combined with the dimension reduction method. Hence, the proposed characteristic timescale model was valuable in providing good initial conditions for finite-rate based combustion models and in improving the efficiency and robustness of spray combustion simulations. 
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