| Citation: | LIU Tantao, GAO Limin, FENG Xudong. Laws and prediction of axial compressor performance map based on data-driven[J]. Journal of Aerospace Power, 2021, 36(5): 1072-1082. doi: 10.13224/j.cnki.jasp.2021.05.018 |
| [1] |
DIXON S L,HALL C A.Fluid mechanics and thermodynamics of turbomachinery[M].7th ed.Oxford,UK:Butterworth-Heinemann,2014.
|
| [2] |
王占学,王永杰,乔渭阳,等.涡扇发动机低转速部件特性扩展和风车状态性能模拟[J].推进技术,2006,27(2):146-149,181. WANG Zhanxue,WANG Yongjie,QIAO Weiyang,et al.Extrapolating component maps into the low speed and simulation of windmilling performance of turbofan engine[J].Journal of Propulsion Technology,2006,27(2):146-149,181.(in Chinese)
|
| [3] |
TSOUTSANIS E,LI Y G,PILIDIS P,et al.Part-load performance of gas turbines:Part Ⅰ a novel compressor map generation approach suitable for adaptive simulation[R].Mumbai,Maharashtra,India:ASME Gas Turbine India Conference,2012.
|
| [4] |
郑洪涛,潘福敏,杨仁.基于面向对象方法的压气机性能计算[J].航空动力学报,2014,29(1):140-145. ZHENG Hongtao,PAN Fumin,YANG Ren.Performance calculation of compressor based on object-oriented method[J].Journal of Aerospace Power,2014,29(1):140-145.(in Chinese)
|
| [5] |
施洋,屠秋野,严红明,等.一种航空发动机全状态性能模型[J].航空动力学报,2017,32(2):373-381. SHI Yang,TU Qiuye,YAN Hongming,et al.A full states performance model for aero engine[J].Journal of Aerospace Power,2017,32(2):373-381.(in Chinese)
|
| [6] |
李枚媛,曾德堂,张永军,等.压气机低转速特性外推法改进研究[J].燃气轮机技术,2016,29(3):11-16. LI Meiyuan,ZENG Detang,ZHANG Yongjun,et al.Research on improvement of extrapolating low speed characteristics of compressor[J].Gas Turbine Technology,2016,29(3):11-16.(in Chinese)
|
| [7] |
KURZKE J.Correlations hidden in compressor maps[R].ASME Paper GT2011-45519,2011.
|
| [8] |
KURZKE J.Component map extension theoretical considerations and practical advices[R].GPPS (Global Power and Propulsion Society)-CH-2020-0005,2020.
|
| [9] |
房友龙,刘东风,贺星武,等.压气机特性曲线精确分步拟合方法研究[J].燃气涡轮试验与研究,2019,32(2):21-27. FANG Youlong,LIU Dongfeng,HE Xingwu,et al.Research on the precise step fitting method of compressor characteristic map[J].Gas Turbine Experiment and Research,2019,32(2):21-27.(in Chinese)
|
| [10] |
TSOUTSANIS E,MESKIN N,BENAMMAR M,et al.A component map tuning method for performance prediction and diagnostics of gas turbine compressors[J].Applied Energy,2014,135(12):572-585.
|
| [11] |
ZAGOROWSKA M,THORNHILL N.Compressor map approximation using Chebyshev polynomials[R].Valletta,Malta:the 25th Mediterranean Conference on Control and Automation (MED),2017.
|
| [12] |
黄伟,常俊,孙智滨.基于 MEA-BP 神经网络的压气机特性曲线预测[J].重庆理工大学学报(自然科学),2019,33(2):67-74. HUANG Wei,CHANG Jun,SUN Zhibin.Characteristic curve prediction of compressor based on MEA-BP neural network[J].Journal of Chongqing University of Technology (Natural Science),2019,33(2):67-74.(in Chinese)
|
| [13] |
蒋爱武,谢寿生.基于支持向量机和粒子群算法的压气机特性计算[J].航空动力学报,2010,25(11):2571-2577. JIANG Aiwu,XIE Shousheng.Method to achieving compressor characteristics based on support vector machine (SVM) and particle swarm optimization (PSO)[J].Journal of Aerospace Power,2010,25(11):2571-2577.(in Chinese)
|
| [14] |
饶高,苏三买,翟向博.指数外推法和支持向量机相结合的压气机特性扩展方法[J].航空动力学报,2017,32(3):749-755. RAO Gao,SU Sanmai,ZHAI Xiangbo.Method of compressor characteristic extension combining exponent extrapolation method with support vector machine[J].Journal of Aerospace Power,2017,32(3):749-755.(in Chinese)
|
| [15] |
MIKHAILOVA A B,AKHMEDZYANOV D A,AKHMETOV Y M,et al.Joint prediction of aircraft gas turbine engine axial flow compressor off-design performance and surge line based on the expanded method of generalized functions[J].Russian Aeronautics,2014,57(3):291-296.
|
| [16] |
AGRAWAL R K,YUNIS M.A generalized mathematical model to estimate gas turbine starting characteristics[R].ASME Paper 81-GT-202,1981.
|
| [17] |
STEVENSON J D,SARAVANAMUTTOO H I H.Simulating indirect thrust measurement methods for high-bypass turbofans[J].Journal of Engineering for Gas Turbines and Power,1995,117(1):38-46.
|
| [18] |
GOSTELOW J P,KRABACHER K W,SMITH L H.Performance comparisons of high Mach number compressor rotor blading[R].NASA-CR-1256,1968.
|
| [19] |
BLANCO R E,HALL C A,CRICHTON D.Challenges in the silent aircraft engine design[R].AIAA 2007-454,2007.
|
| [20] |
SULAM D H,KEENAN M J,FLYNN J T.Single-stage evaluation of highly-loaded high-Mach-number compressor stages:Ⅱ data and performance,multiple-circular-arc rotor[R].NASA-CR-72694,1970.
|
| [21] |
CONVERSE G L.Extended parametric representation of compressor fans and turbines:Volume Ⅲ MODFAN user’s manual[R].NASA-CR-174647,1984.
|
| [22] |
CHENG R,ULTICH W,LAN F,et al.Design and test demonstration of the JET01 six-stage high-pressure compressor[R].ISABE(International Society for Air Breathing Engines) 2007-1184,2007.
|