首页> 外文期刊>Combustion and Flame >Large eddy simulation of a reacting spray flame with multiple realizations under compression ignition engine conditions
【24h】

Large eddy simulation of a reacting spray flame with multiple realizations under compression ignition engine conditions

机译:压缩点火发动机工况下具有多种实现的反应喷雾火焰的大涡模拟

获取原文
获取原文并翻译 | 示例
       

摘要

An n-dodecane spray flame (Spray A from Engine Combustion Network) was simulated using a 3 function combustion model along with a dynamic structure large eddy simulation (LES) model to evaluate its performance at engine-relevant conditions and to understand the transient behavior of this turbulent flame. The liquid spray was treated with a traditional Lagrangian method and the gas-phase reaction was modeled using a 8 function combustion model. A 103-species skeletal mechanism was used for the n-dodecane chemical kinetic model. Significantly different flame structures and ignition processes are observed for the LES compared to those of Reynolds-averaged Navier-Stokes (RANS) predictions. The LES data suggests that the first ignition initiates in a lean mixture and propagates to a rich mixture, and the main ignition happens in the rich mixture, preferably less than 0.14 in mixture fraction space. LES was observed to have multiple ignition spots in the mixing layer simultaneously while the main ignition initiates in a clearly asymmetric fashion. The temporal flame development also indicates the flame stabilization mechanism is auto-ignition controlled. Soot predictions by LES present much better agreement with experiments compared to RANS, both qualitatively and quantitatively. Multiple realizations for LES were performed to understand the realization to realization variation and to establish best practices for ensemble-averaging diesel spray flames. The relevance index analysis suggests that an average of 5 and 6 realizations can reach 99% of similarity to the target average of 16 realizations on the mixture fraction and temperature fields, respectively. However, more realizations are necessary for the hydroxide (OH) and soot mass fractions due to their high fluctuations. (C) 2015 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
机译:使用三功能燃烧模型和动态结构大涡模拟(LES)模型对正十二烷喷雾火焰(发动机燃烧网络的喷雾A)进行了仿真,以评估其在发动机相关条件下的性能并了解发动机的瞬态行为。这湍急的火焰。用传统的拉格朗日方法对液体喷雾进行处理,并使用8函数燃烧模型对气相反应进行建模。 103种骨骼机制用于正十二烷化学动力学模型。与雷诺平均的Navier-Stokes(RANS)预测相比,LES的火焰结构和点火过程明显不同。 LES数据表明,第一次点火是在稀混合气中引发并传播到浓混合气,而主点火发生在浓混合气中,最好在混合分数空间内小于0.14。观察到LES在混合层中同时具有多个点火点,而主点火以明显不对称的方式引发。短暂的火焰发展也表明火焰稳定机制是自动点火控制的。与RANS相比,LES在定性和定量方面对煤烟的预测与实验的一致性更好。进行了LES的多个实现,以了解实现变化的实现并建立总体平均柴油喷雾火焰的最佳实践。相关指数分析表明,在混合分数和温度场上,平均5个实现和6个实现可以分别达到16个实现的目标平均值的99%相似度。但是,由于氢氧化物(OH)和烟灰的质量分数波动大,因此需要更多的认识。 (C)2015年燃烧研究所。由Elsevier Inc.出版。保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号