航空发动机数值缩放技术的研究进展 *

推进技术 ›› 2018, Vol. 39 ›› Issue (7): 1441-1454.

• 综述 • 下一篇

航空发动机数值缩放技术的研究进展 *

王占学,宋甫,周莉,张晓博,张明阳

西北工业大学动力与能源学院，陕西西安 710129,西北工业大学动力与能源学院，陕西西安 710129,西北工业大学动力与能源学院，陕西西安 710129,西北工业大学动力与能源学院，陕西西安 710129,西北工业大学动力与能源学院，陕西西安 710129

发布日期:2021-08-15
基金资助:
国家自然科学基金( 51576163)。

Research Progressin Numerical Zooming Technologyof Aero-Engine

School of Power and Energy，Northwestern Polytechnical University，Xi’an 710129，China,School of Power and Energy，Northwestern Polytechnical University，Xi’an 710129，China,School of Power and Energy，Northwestern Polytechnical University，Xi’an 710129，China,School of Power and Energy，Northwestern Polytechnical University，Xi’an 710129，China and School of Power and Energy，Northwestern Polytechnical University，Xi’an 710129，China

Published:2021-08-15

摘要/Abstract

摘要： 航空发动机整机和部件仿真是航空发动机设计与研究的常规手段，是短周期研制先进水平航空发动机的重要环节和手段。数值缩放技术可以将基于高精度模型求解的部件特性用于整机性能分析，在有限的计算资源下提高航空发动机整机仿真精度，是实现航空发动机整机和部件高精度仿真的关键技术之一。同时数值缩放技术可以使部件设计在航空发动机整机环境中得到快速、全面的评估与分析，提高航空发动机设计的可信度，降低开发成本与周期。梳理了国内外航空发动机数值仿真技术的发展趋势，回顾了数值缩放技术的发展及在实际研究中的应用情况，分析、总结了数值缩放技术的三种实现方法及现阶段数值缩放技术应用中存在的问题，提出了我国数值缩放技术发展需重点关注的方向。

关键词: 航空发动机；数值仿真；高精度；变精度分析；数值缩放；数值缩放方法

Abstract: The numerical simulation is a routine method for the research and design of the system and com.ponents of aero-engine and is important for developing advanced aero-engines in short period. Zooming technolo.gy is one of the key technologies to realize high precision simulation of aero-engine and components，which inte. grates the high-fidelity performance characteristics of an aero-engine component into aero-engine system perfor.mance analysis，and can improve the accuracy of system and components simulation of aero-engine with limitedcomputation resources. In addition，the components design can be analyzed and evaluated quickly and thorough.ly in the aero-engine environment with zooming technology which is beneficial to improving the design reliabilityand reducing the cost and period of aero-engine development. The development trend of aero-engine numericalsimulation technology in China and abroad is briefly introduced. The progress and applications of zooming tech.nology are reviewed. Three different zooming strategies are analyzed and the problems unresolved are discussed.The future efforts for research on zooming technology are also proposed.

Key words: Aero-engine； Numerical simulation； High fidelity； Variable complexity analysis； Zoom. ing；Zooming strategy

王占学,宋甫,周莉,张晓博,张明阳. 航空发动机数值缩放技术的研究进展 *[J]. 推进技术, 2018, 39(7): 1441-1454.

WANG Zhan-xue,SONG Fu,ZHOU Li,ZHANG Xiao-bo,ZHANG Ming-yang. Research Progressin Numerical Zooming Technologyof Aero-Engine[J]. Journal of Propulsion Technology, 2018, 39(7): 1441-1454.

参考文献

[1] Claus R W,Lavelle T,Townsend S,et al.Variable Fi.delity Analysis of Complete Engine Systems[R].AIAA 2007-5042.
[2] Nichols L D,Chamis C C.Numerical Propulsion Sys.tem Simulation: An Interdisciplinary Approach[R].AIAA 91-3554.
[3] Claus R W,Evans A L,Lylte J K,et al.Numerical Pro.pulsion System Simulation[J].Computing Systems in Engineering,1991,2(4): 357-364.
[4] Lytel J,Follen G,Naiman C,et al.2001 Numerical Propulsion System Simulation Review[R].NASA / TM-2002-211197.
[5] Gleen Research Center.Research & Technology 2001[R].NASA/TM-2002-211333.
[6] Lytle J K.Multi-Fidelity Simulations of Air BreathingPropulsion Systems[R].AIAA 2006-4967.
[7] Witherell R E.Design Point Turbine Engine Perfor.mance Program[R].AFAPL-TR-68-88.
[8] Koenibg R W,Fishbach L H.GENENG: A Program forCalculating Design and Off-Design Performance for Tur.bojet and Turbofan Engines[R].NASA/TN-D-6552.
[9] Sellers J F,Daniele C J.DYNGEN: A Program for Cal.culating Steady-State and Transient Performance of Tur.bojet and Turbofan Engines[R].NASA/TN-D-7901.
[10] Fishbach L H,Caddy M J.NNEP: The Navy NASA En.gine Program[R].NASA/TM-X-71857.
[11] Reed J A,Afjeh A A.An Object-Oriented Frameworkfor Distributed Computational Simulation of AerospacePropulsion Systems[C].Santa Fe: Proceedings of the 4th USENIX Conference on Object-Oriented Technologies and Systems(COOTS),1998.
[12] Vissere W P J,Broomhead M J.GSP: A Generic Ob. ject-Oriented Gas Turbine Simulation Environment[R].NLR-TP-2000-267.
[13] Byerley A R,Rouser K P,O’Dowd D O.ExploringGasTurb 12 for Supplementary Use on an Introductory Propulsion Design Project[R].ASME GT 2017-63465.
[14] Bala A.Poly-Dimensional Gas Turbine System Model.ing and Simulation[D].England: Cranfield University, 2007.
[15] Alexiou A,Tsalavoutas T.Introduction to Gas Turbine Modelling with PROOSIS[M].Madrid: Agrupados Internacional(EAI),2011.Empresarios
[16] Lytle J K.The Numerical Propulsion System Simulation:A Multidisciplinary Design System for Aerospace Vehi.cles[R].NASA/TM-1999-209194.
[17] National Aeronautics and Space Administration.NPSS User Guide[M].Cleveland: NASA Glenn Research Cen. ter,2008.
[18] Lytle J K.The Numerical Propulsion System Simulation: An Overview[R].NASA/TM-2000-209915.
[19] Charles L.An Overview of Three Approaches to Multi.disciplinary Aeropropulsion Simulation[R].NASA/TM-107443.
[20] Evans A L,Follen C,Naiman C,et.al.Numerical Pro. pulsion System’s National Cycle Program[R].AIAA 98-3113.
[21] Alexiou A,Baalbergen E H,Koggenhop O,et al.Ad.vanced Capabilities for Gas Turbine Engine Performance Simulation[R].ASME GT 2007-27086.
[22] Pachidis V,Pilidis P,Guindeuil G,et al.A Partially Integrated Approach to Component Zooming Using Com.putational Fluid Dynamics[R].ASME GT 2005-68457.
[23] Pachidis V,Pilidis P,Talhouarn F,et al.A Fully Inte.grated Approach to Component Zooming Using Computa.tional Fluid Dynamics[J].Journal of Engineering for Gas Turbines and Power,2006,128(3): 579-584.
[24] Pachidis V,Pilidis P,Alexander T,et al.Advanced Performance Simulation of a Turbofan Engine Intake[J].Journal of Propulsion and Power,2006,22(1): 201-205.
[25] Pachidis V,Pilidis P,Templalexis I,et al.A De-cou.pled Approach to Component High-Fidelity Analysis Us.ing Computational Fluid Dynamics[J].Journal of Aero.space Engineering,2007,221(1): 105-113.
[26] Pachidis V,Pilidis P,Texeira J,et al.A Comparison of Component Zooming Simulation Strategies Using Streamline Curvature[J].Journal of Aerospace Engineer. ing,2007,221(1): 1-15.
[27] 何谦 .航空发动机数值仿真工程应用研究[ D].成都:电子科技大学, 2008.
[28] Follen G,Aubuchon M.Numerical Zooming Between aNPSS Engine System Simulation and a One-Dimension.al High Compressor Analysis Code[R].NASA / TM-2000-209913.
[29] Sampath R,Irani R,Balasubramaniam M,et al.High Fidelity System Simulation of Aerospace Vehicles UsingNPSS[R].AIAA 2004-371.
[30] Connolly J W,Kopasakis G.Computational Fluid Dy.namics Modeling of a Supersonic Nozzle and Integration into a Variable Cycle Engine Model[R].AIAA 2014-3687.
[31] Allison D,Alyanak E.Development of Installed Propul.sion Performance Model for High-Performance AircraftConceptual Design[R].AIAA 2014-2725.
[32] Melloni L,Kotsiopoutlos P,Jackson A,et al.MilitaryEngine Response to Compressor Inlet Stratified Pressure Distortion by an Integrated CFD Analysis[R].ASME GT 2006-90805.

航空发动机数值缩放技术的研究进展 *

Research Progressin Numerical Zooming Technologyof Aero-Engine

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