AECSC-JASMIN湍流燃烧仿真软件研发和检验

doi:10.7527/S1000-6893.2021.25003

Abstract

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

CLC Number:

V231.2

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.

References

[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.

Development and testing of AECSC-JASMIN turbulent combustion simulation software

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Binbin ZHAO, Heng ZHANG, Jie LI. Review of numerical simulation on complex separated flow of iced airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627211-627211.
[2]	XIAHOU Tangfan, CHEN Jiangtao, SHAO Zhidong, WU Xiaojun, LIU Yu. Model validation metrics for CFD numerical simulation under aleatory and epistemic uncertainty [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 25716-025716.
[3]	YANG Jiankai, GU Dongdong, GE Qing, TAN Chenchen, WEN Yu. Support layout and precise forming mechanism of aluminum alloy for laser additive manufacturing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(4): 525331-525331.
[4]	JIANG Youxu, LI Jie, YANG Zhao. Data correction method of wind tunnel test for verification aircraft with laminar wing section [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526814-526814.
[5]	WANG Hao, ZHONG Min, HUA Jun, ZHONG Hai, YANG Tihao, WANG Meng, LEI Guodong. Simulation and experiment of natural laminar flow flight test wing glove [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526785-526785.
[6]	DUAN Junyi, TONG Fulin, LI Xinliang, LIU Hongwei. Decomposition of mean friction drag in compression-expansion turbulent boundary layer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 625915-625915.
[7]	SHEN Pengfei, LIU Pengxin, SUN Dong, YUAN Xianxu. Statistical characteristics of skin friction of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach 6 [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 626005-626005.
[8]	LIU Pengxin, YUAN Xianxu, LIANG Fei, LI Chen, SUN Dong. Quadrant decomposition analysis of fluctuations in high-temperature turbulent boundary layer with chemical non-equilibrium [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726338-726338.
[9]	BAO Jun, WANG Yu, NIU Qian, ZHU Xidong, CHENG Jianjie. Influencing parameters and film flow mechanism of spray droplet impacting liquid film [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726360-726360.
[10]	CHEN Chongpei, LIANG Jianhan, GUAN Qingdi, GAO Tianyun. Conservative compressible one-dimensional turbulence method and its application in supersonic scalar mixing layer [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726364-726364.
[11]	LI Qing, TU Guohua, YU Zhaosheng, LIN Zhaowu, LI Tingting, YUAN Xianxu. Inertial particle transport in non-uniform accelerated flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726390-726390.
[12]	LI Chengcheng, LI Fang, YANG Bin, WANG Ying. Numerical investigation of nozzle flow separation control using plasma actuation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(7): 124547-124547.
[13]	HE Chuangxin, DENG Zhiwen, LIU Yingzheng. Turbulent flow data assimilation and its applications [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(4): 524704-524704.
[14]	LIU Zongxing, LIU Jun, LI Weina. Dynamic response and failure of typical fuselage structure under blast impact load [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 224252-224252.
[15]	SUN Dong, LIU Pengxin, SHEN Pengfei, TONG Fulin, GUO Qilong. Direct numerical simulation of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach number 6 [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 124681-124681.