AECSC-JASMIN湍流燃烧仿真软件研发和检验

doi:10.7527/S1000-6893.2021.25003

多相流与反应流的机理、模型及其调控技术专栏

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

AECSC-JASMIN湍流燃烧仿真软件研发和检验

王方¹, 王煜栋¹, 姜胜利^2,3, 陈军², 唐军⁴, 徐华胜⁴, 李象远⁵, 邢竞文¹, 高东硕¹, 金捷¹

1. 北京航空航天大学能源与动力工程学院, 北京 100191;
2. 北京应用物理与计算数学研究所, 北京 100088;
3. 中物院高性能数值模拟软件中心, 北京 100088;
4. 中国燃气涡轮研究院, 成都 610599;
5. 四川大学化学工程学院, 成都 610065

收稿日期:2020-11-26 修回日期:2021-01-05 发布日期:2021-04-29
通讯作者: 王方 E-mail:fwang@buaa.edu.cn
基金资助:
国家重点研发计划（2017YFB0202400，2017YFB0202402）

Development and testing of AECSC-JASMIN turbulent combustion simulation software

WANG Fang¹, WANG Yudong¹, JIANG Shengli^2,3, CHEN Jun², TANG Jun⁴, XU Huasheng⁴, LI Xiangyuan⁵, XING Jingwen¹, GAO Dongshuo¹, JIN Jie¹

1. School of Energy and Power Engineering, Beihang University, Beijing 100191, China;
2. Institute of Applied Physics and Computational Mathematics, Beijing 100088, China;
3. CAEP Software Center for High Performance Numerical Simulation, Beijing 100088, China;
4. China Gas Turbine Establishment, Chengdu 610599, China;
5. School of Chemical Engineering, Sichuan University, Chengdu 610065, China

Received:2020-11-26 Revised:2021-01-05 Published:2021-04-29
Supported by:
National Key Research and Development Program of China (2017YFB0202400, 2017YFB0202402)

摘要/Abstract

摘要： 航空发动机燃烧室几何结构复杂，湍流和化学反应存在强烈非线性相互作用，需要对流动和燃烧及其相互作用进行高精度高时空分辨率的刻画，目前燃烧室湍流燃烧数值模拟仍然是高难度的瓶颈问题之一。介绍了由北京航空航天大学航空发动机数值仿真研究中心、北京应用物理与计算数学研究所和中国工程物理研究院高性能数值模拟软件中心联合研发的AECSC-JASMIN软件主要框架、算法以及针对该软件的算例检验。在Sandia射流火焰、支板火焰和单头部燃烧室检验算例中，对比实验数据，射流和支板火焰预测结果与实验值一致；支板算例的平均相对误差在15%之内；单头部燃烧室模拟结果符合物理实际，总压损失与实验值基本吻合。说明AECSC-JASMIN软件可用于复杂结构高分辨率高精度湍流燃烧数值模拟。

关键词: 航空发动机燃烧室, 大涡模拟(LES), 概率密度函数输运方程湍流燃烧模型(TPDF), AECSC软件, JASMIN框架, 数值模拟

Abstract: The complex geometry of the aero-engine combustion chambers and the strong nonlinear interaction between turbulence and chemical reactions require high precision characterization of the flow, combustion, and their interaction with high space-time resolution. Currently, the difficulty in numerical simulation of turbulent combustion in the combustion chamber remains one of the bottleneck problems. This article will introduce the main algorithm of the AECSC-JASMIN software, which is jointly developed by the Aeroengine Numerical Simulation Research Center of Beihang University, Institute of Applied Physics and Computational Mathematics, and CAEP Software Center for High-Performance Numerical Simulation, as well as the example verification of the software. It will be tested with Sandia`s jet flame, concave strut flame-holder, and single-head combustion chamber. Compared with the experimental data, the prediction results of the jet and concave strut flame-holder are consistent with the experimental values, with an average relative error within 15%. The simulation results of the single-head combustion chamber conform to the physical reality, and the total pressure loss is consistent with the experimental value. Therefore, AECSC-JASMIN software can be used for numerical simulation of high-resolution and high-precision turbulent combustion in complex structures.

Key words: aero-engine combustors, Large Eddy Simulation (LES), Transport Probability Density Function (TPDF), AECSC, JASMIN framework, numerical simulation

中图分类号:

V231.2

王方, 王煜栋, 姜胜利, 陈军, 唐军, 徐华胜, 李象远, 邢竞文, 高东硕, 金捷. AECSC-JASMIN湍流燃烧仿真软件研发和检验[J]. 航空学报, 2021, 42(12): 625003-625003.

WANG Fang, WANG Yudong, JIANG Shengli, CHEN Jun, TANG Jun, XU Huasheng, LI Xiangyuan, XING Jingwen, GAO Dongshuo, JIN Jie. Development and testing of AECSC-JASMIN turbulent combustion simulation software[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 625003-625003.

参考文献

[1] JONES W P, MARQUIS A J, WANG F. Large eddy simulation of a premixed propane turbulent bluff body flame using the Eulerian stochastic field method[J]. Fuel, 2015, 140:514-525.
[2] 曾家, 金捷, 张晟, 等. 基于LES-PDF方法的双旋流模型燃烧室数值模拟[J]. 气体物理, 2019, 4(5):52-64. ZENG J, JIN J, ZHANG S, et al. Numerical simulation of double-swirled model combustor based on LES-PDF[J]. Physics of Gases, 2019, 4(5):52-64(in Chinese).
[3] WANG F, LIU R, DOU L, et al. A dual timescale model for micro-mixing and its application in LES-TPDF simulations of turbulent nonpremixed flames[J]. Chinese Journal of Aeronautics, 2019, 32(4):875-887.
[4] 任健, 魏军侠, 曹小林. 基于JASMIN框架的辐射流体与粒子输运耦合计算[J]. 计算物理, 2012, 29(2):205-212. REN J, WEI J X, CAO X L. Composition computation of radiation hydrodynamics and particle transport based on JASMIN[J]. Chinese Journal of Computational Physics, 2012, 29(2):205-212(in Chinese).
[5] 程汤培, 雷伟, 衷斌, 等. 三维中子/光子输运S_N程序的并行重构[J]. 核动力工程, 2014, 35(增刊2):147-150. CHENG T P, LEI W, ZHONG B, et al. Reconstruction and parallelization of 3D SN program for neutron/photon transport[J]. Nuclear Power Engineering, 2014, 35(Sup 2):147-150(in Chinese).
[6] 曹小林, 莫则尧, 刘旭, 等. 基于JASMIN框架的快速多极子并行解法器[J]. 中国科学:信息科学, 2010, 40(9):1187-1196. CAO X L, MO Z Y, LIU X, et al. A fast multipole parallel resolver based on JASMIN framework[J]. Scientia Sinica (Informationis), 2010, 40(9):1187-1196(in Chinese).
[7] 左风丽, 刘旭, 张宝印, 等. 基于JASMIN三维势场快速多极子算法的并行实现[J]. 计算物理, 2013, 30(1):140-147. ZUO F L, LIU X, ZHANG B Y, et al. Parallel implementation of fast multipole methods for three-dimensional potential fields on JASMIN[J]. Chinese Journal of Computational Physics, 2013, 30(1):140-147(in Chinese).
[8] 莫妲, 程明, 万斌, 等. 三旋流燃烧室的数值模拟与试验[J]. 航空动力学报, 2017, 32(11):2568-2575. MO D, CHENG M, WAN B, et al. Numerical simulation and experiment of triple swirler combustor[J]. Journal of Aerospace Power, 2017, 32(11):2568-2575(in Chinese).
[9] 丁勇能, 田勇, 王波, 等. 某重型燃气轮机DLN燃烧室数值模拟-热态分析[J]. 燃气轮机技术, 2019, 32(2):40-43, 51. DING Y N, TIAN Y, WANG B, et al. Numerical investigation of the DLN combustor of a heavy gas turbine-hot flow field analysis[J]. Gas Turbine Technology, 2019, 32(2):40-43, 51(in Chinese).
[10] 刘晓恒, 周成华, 宋满祥, 等. 基于通流方法的某涡喷发动机整机数值仿真[J]. 航空学报, 2020, 41(1):123199. LIU X H, ZHOU C H, SONG M X, et al. Overall simulation of a turbojet engine based on throughflow method[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(1):123199(in Chinese).
[11] 王年华, 常兴华, 赵钟, 等. 非结构CFD软件MPI+OpenMP混合并行及超大规模非定常并行计算的应用[J]. 航空学报, 2020, 41(10):123859. WANG N H, CHANG X H, ZHAO Z, et al. Implementation of hybrid MPI+OpenMP parallelization on unstructured CFD solver and its applications in massive unsteady simulations[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10):123859(in Chinese).
[12] ZHOU Y, LE J L, HUANG Y. LES of combustion flow field in a practical aeroengine combustor with two-stage counter-rotating swirler[J]. Journal of Propulsion Technology, 2018, 39(7):1576-1589.
[13] JABERI F A, COLUCCI P J, JAMES S, et al. Filtered mass density function for large-eddy simulation of turbulent reacting flows[J]. Journal of Fluid Mechanics, 1999, 401:85-121.
[14] PESKIN C S. Flow patterns around heart valves:A numerical method[J]. Journal of Computational Physics, 1972, 10(2):252-271.
[15] PESKIN C S. Numerical analysis of blood flow in the heart[J]. Journal of Computational Physics, 1977, 25(3):220-252.
[16] PESKIN C S. The immersed boundary method[J]. Acta Numerica, 2002, 11:479-517.
[17] LUTZ A E, KEE R J, GRCAR J F, et al. OPPDIF:A Fortran program for computing opposed-flow diffusion flames:SAND-96-8243[R]. Oak Ridge:Office of Scientific and Technical Information (OSTI), 1997.
[18] BARLOW R S, FRANK J H. Effects of turbulence on species mass fractions in methane/air jet flames[J]. Symposium (International) on Combustion, 1998, 27(1):1087-1095.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

AECSC-JASMIN湍流燃烧仿真软件研发和检验

Development and testing of AECSC-JASMIN turbulent combustion simulation software

RichHTML

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	赵宾宾, 张恒, 李杰. 翼型结冰状态复杂分离流动数值模拟综述[J]. 航空学报, 2023, 44(1): 627211-627211.
[2]	夏侯唐凡, 陈江涛, 邵志栋, 吴晓军, 刘宇. 随机和认知不确定性框架下的CFD模型确认度量综述[J]. 航空学报, 2022, 43(8): 25716-025716.
[3]	杨建凯, 顾冬冬, 葛庆, 檀晨晨, 文雨. 铝合金激光增材制造支撑布局及精确成形机制[J]. 航空学报, 2022, 43(4): 525331-525331.
[4]	姜有旭, 李杰, 杨钊. 某层流机翼验证机风洞试验数据修正方法[J]. 航空学报, 2022, 43(11): 526814-526814.
[5]	段俊亦, 童福林, 李新亮, 刘洪伟. 压缩-膨胀湍流边界层平均摩阻分解[J]. 航空学报, 2022, 43(1): 625915-625915.
[6]	刘朋欣, 袁先旭, 孙东, 傅亚陆, 李辰. 高温化学非平衡湍流边界层直接数值模拟[J]. 航空学报, 2022, 43(1): 124877-124877.
[7]	沈鹏飞, 刘朋欣, 孙东, 袁先旭. 马赫6柱-裙构型激波/湍流边界层干扰摩阻统计特性[J]. 航空学报, 2022, 43(1): 626005-626005.
[8]	刘朋欣, 袁先旭, 梁飞, 李辰, 孙东. 高温化学非平衡湍流边界层脉动量象限分析[J]. 航空学报, 2021, 42(S1): 726338-726338.
[9]	鲍俊, 王瑜, 牛潜, 朱锡冬, 程建杰. 喷雾液滴撞击液膜影响参数及流动机理分析[J]. 航空学报, 2021, 42(S1): 726360-726360.
[10]	陈崇沛, 梁剑寒, 关清帝, 高天运. 守恒型可压缩一维湍流方法及其在超声速标量混合层中的应用[J]. 航空学报, 2021, 42(S1): 726364-726364.
[11]	李青, 涂国华, 余钊圣, 林昭武, 李婷婷, 袁先旭. 惯性颗粒在非均匀加速流中的输运问题[J]. 航空学报, 2021, 42(S1): 726390-726390.
[12]	李成成, 李芳, 杨斌, 王莹. 等离子体激励抑制喷管分离流动数值模拟[J]. 航空学报, 2021, 42(7): 124547-124547.
[13]	刘宗兴, 刘军, 李维娜. 爆炸冲击载荷下典型机身结构动响应及破坏[J]. 航空学报, 2021, 42(2): 224252-224252.
[14]	孙东, 刘朋欣, 沈鹏飞, 童福林, 郭启龙. 马赫数6柱-裙激波/边界层干扰直接模拟[J]. 航空学报, 2021, 42(12): 124681-124681.
[15]	崔笑蕾, 詹梅, 高鹏飞, 李锐, 王贤贤, 雷煜东, 马飞, 张洪瑞. 虑及板坯几何和性能波动的薄壁件塑性成形数值模拟研究进展[J]. 航空学报, 2021, 42(10): 525145-525145.