基于时间推进的涡扇发动机整机通流数值模拟

doi:10.13675/j.cnki. tjjs. 190144

推进技术 ›› 2019, Vol. 40 ›› Issue (10): 2190-2197.DOI: 10.13675/j.cnki. tjjs. 190144

基于时间推进的涡扇发动机整机通流数值模拟

杨晨¹,吴虎¹,杨金广²,王大磊³

1.西北工业大学动力与能源学院;2.大连理工大学能源与动力学院;3.北京动力机械研究所，北京;100074

发布日期:2021-08-15
作者简介:杨晨，博士生，研究领域为叶轮机械计算流体力学。E-mail：yangchen@mail.nwpu.edu.cn
基金资助:
国家自然科学基金青年项目 51606026;国家重点研发计划 2016YFB0600100国家自然科学基金青年项目（51606026）；国家重点研发计划（2016YFB0600100）。

Numerical Investigation of Turbofan Engine Based onTime-Marching Throughflow Method

1.School of Power and Energy,Northwestern Polytechnical University,Xi’an 710129,China;2.School of Energy and Power Engineering,Dalian University of Technology,Dalian 116024,China;3.Beijing Institute of Power Machinery,Beijing 10074,China

Published:2021-08-15

摘要/Abstract

摘要： 为实现航空发动机整机流场与性能快速分析，基于准三维控制方程模型，开发了整机通流数值模拟程序。程序基于计算流体力学理论，并考虑了引气、冷却和喷油等发动机中的物理现象。为模拟叶片对气流偏转作用，推导了一种鲁棒的无粘叶片力模型，同时采用粘性力模型模拟粘性损失效应。采用该程序对某型双轴分排涡扇发动机一个地面试车工况点进行了整机数值仿真，并与实验数据进行了对比验证。结果表明，所发展程序求解稳定，能够自动捕捉激波，并且可以快速获得完全收敛的航空发动机整机准三维流场，单工况点计算时长不大于30min。其中计算截面平均参数与实验测量偏差不大于8%，符合工程应用精度需求。

关键词: 航空发动机;整机模拟;时间推进;通流;叶片力

Abstract: In order to achieve a fast simulation of flow filed and performance of a whole aero engine, a throughflow program is developed based on the quasi-three dimensional (Q3D) governing equations model. In this program, computational fluid dynamics (CFD) techniques are used to solve the governing equation, and many physical phenomena are modeled, including air bleeding, cooling and fuel injection etc. A robust inviscid blade force model is derived in order to obtain the flow deflection inside the blades, and a viscous force model is utilized to simulate the viscous loss effects. With this program, simulation for a dual-spool, separate exhaust turbo-fan engine at a ground test operation point is conducted, and computational results are compared with the experiment data. It is shown that the developed program is stable, capable of automatically capturing shock waves, and able to quickly obtain completely converged Q3D flow field of the whole aero engine, the calculation of which costs less than 30min on one operating point. The maximum error of area-averaged characteristic parameters is less than 8% compared to all test data, meeting the accuracy requirements of engineering applications.

Key words: Aero engine;Whole engine simulation;Time-marching;Throughflow;Blade force

杨晨,吴虎,杨金广,王大磊. 基于时间推进的涡扇发动机整机通流数值模拟[J]. 推进技术, 2019, 40(10): 2190-2197.

YANG Chen¹,WU Hu¹,YANG Jin-guang²,WANG Da-lei³. Numerical Investigation of Turbofan Engine Based onTime-Marching Throughflow Method[J]. Journal of Propulsion Technology, 2019, 40(10): 2190-2197.

参考文献

[1] 曹建国. 航空发动机仿真技术研究现状、挑战和展望[J]. 推进技术, 2018， 39(5): 961-970. (CAO Jian-guo. Status， Challenges and Perspectives of Aero-Engine Simulation Technology[J]. Journal of Propulsion Technology， 2018， 39(5): 961-970.)
[2] Wu C H. A General Theory of Three-Dimensional Flow in Subsonic and Supersonic Turbomachines of Axial-， Radial-， and Mixed-Flow Types[R]. NACA TN2604， 1952.
[3] Novak R A. Streamline Curvature Computing Procedures for Fluid-Flow Problems[J]. Journal of Engineering for Power， 1967， 89(4): 478-490.
[4] Marsh H. A Digital Computer Program for the Through-Flow Fluid Mechanics in an Arbitrary Turbomachine Using a Matrix Method[M]. UK: Ministry of Aviation， 1966.
[5] Godunov S K. A Difference Method for Numerical Calculation of Discontinuous Solutions of the Equations of Hydrodynamics[J]. Matematicheskii Sbornik， 1959， 89(3): 271-306.
[6] Jameson A， Schmidt W， Turkel E. Numerical Solution of the Euler Equations by Finite Volume Methods Using Runge Kutta Time Stepping Schemes[R]. AIAA81-1259.
[7] Denton J D， Dang T Q. The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines[R]. ASME 90-GT-019.
[8] Medic G， Kalitzin G， You D， et al. Integrated RANS/LES Computations of an Entire Gas Turbine Jet Engine[R]. AIAA2007-1117.
[9] Teixeira M， Romagnosi L， Mezine M， et al. A Methodology for Fully-Coupled CFD Engine Simulations， Applied to a Micro Gas Turbine Engine[R]. ASME GT2018-76870.
[10] Hall E， Owen P. Energy Efficient Engine HP/LP Spool Analysis[R]. NASA CR-785， 2008.
[11] Claus R W， Lavelle T， Townsend S， et al. Coupled High-Fidelity Engine System Simulation[R]. 26th ICAS 845， 2008.
[12] Claus R W， Lavelle T， Townsend S， et al. Component Coupled， Full Engine Simulation of a Gas Turbine Engine[R]. AIAA2009-5017.
[13] Turner M G， Reed J A， Ryder R， et al. Multi-Fidelity Simulation of a Turbofan Engine with Results Zoomed into Mini-Maps for a Zero-D Cycle Simulation[R]. ASME GT2004-53956.
[14] Pilet J， Lecordix J L， Garcia-Rosa N， et al. Towards a Fully Coupled Component Zooming Approach in Engine Performance Simulation[R]. ASME GT2011-46320.
[15] Klein C， Reitenbach S， Schoenweitz D， et al. A Fully Coupled Approach for the Integration of 3D-CFD Component Simulation in Overall Engine Performance Analysis[R]. ASME GT2017-63591.
[16] Petrovic M V， Wiedermann A. Fully Coupled Through-flow Method for Industrial Gas Turbine Analysis[R]. ASME GT2015-42111.
[17] 杨金广，王春雪，王大磊，等. 基于时间推进的通流计算方法:现状及展望[J]. 航空学报， 2017， 38(9):58-70.
[18] Baralon S， Eriksson L， Hall U. Validation of a Throughflow Time-Marching Finite-Volume Solver for Transonic Compressors[R]. ASME 98-GT-47.
[19] Pacciani R， Marconcini M， Arnone A. A CFD-Based Throughflow Method with Three-Dimensional Flow Features Modelling[J]. Journal of Turbomachinery， Propusion and Power， 2017， 2(3): 11-20.
[20] Nigmatullin R， Ivanov M. The Mathematical Models of Flow Passage for Gas Turbine Engines and Their Components[R]. AGARD LS-198， 1994.
[21] 季路成，孟庆国，周盛. 叶轮机通流计算的时间推进方法[J]. 航空动力学报， 1999， 14(1): 24-27.
[22] 曹志鹏，刘大响，桂幸民，等. 某小型涡喷发动机二维数值仿真[J]. 航空动力学报， 2009， 24(2): 439-444.
[23] 金东海，桂幸民. 某涡扇发动机考虑级间引气的二维数值模拟[J]. 航空动力学报， 2011， 26(6): 1346-1351.
[24] Hirsch C, Warzee G. A Finite-Element Method for Through Flow Calculations in Turbomachines[R]. ASME 76-FE-12.
[25] Cetin M， Ucer A， Hirsch C， et al. Application of Modified Loss and Deviation Correlations to Transonic Axial Compressors[R]. AGARD R-745， 1987.
[26] 昌中宏，唐海龙. 航空发动机整机二维气动热力数值模拟[J]. 推进技术， 2012， 33(3): 333-337. (CHANG Zhong-hong， TANG Hai-long. Aerothermodynamic Numerical Simulation of Integrated Aero Engine System[J]. Journal of Propulsion Technology， 2012， 33(3): 333-337.)

基于时间推进的涡扇发动机整机通流数值模拟

Numerical Investigation of Turbofan Engine Based onTime-Marching Throughflow Method

PDF

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 0

编辑推荐

Metrics

本文评价