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基于特征时间模型的高效喷雾燃烧数值模拟

Efficient spray combustion simulations using the characteristic timescale model
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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。 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.
作者 尹钰 杨天威 周华 任祝寅 林宏军 尚守堂 YIN Yu;YANG Tianwei;ZHOU Hua;REN Zhuyin;LIN Hongjun;SHANG Shoutang(School of Aerospace Engineering,Tsinghua University,Beijing 100084,China;Institute for Aero Engine,Tsinghua University,Beijing 100084,China;Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang 110015,China)
出处 《航空动力学报》 EI CAS CSCD 北大核心 2023年第1期104-115,共12页 Journal of Aerospace Power
基金 国家自然科学基金(91841302) 国家科技重大专项(2017-Ⅰ-0004-0005)。
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 characteristic time scale model finite-rate combustion model spray combustion combustor efficient initialization implementation
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