论文:2023,Vol:41,Issue(2):363-369
引用本文:
崔佳航, 李江红, 李晓宇, 董素艳, 蔡飞超, 范玮. 一种新型进气畸变设计体系研究[J]. 西北工业大学学报
CUI Jiahang, LI Jianghong, LI Xiaoyu, DONG Suyan, CAI Feichao, FAN Wei. A new intake distortion design system for research[J]. Journal of Northwestern Polytechnical University

一种新型进气畸变设计体系研究
崔佳航1, 李江红1, 李晓宇2, 董素艳1, 蔡飞超1, 范玮1
1. 西北工业大学 动力与能源学院, 陕西 西安 710072;
2. 中国飞行试验研究院, 陕西 西安 710089
摘要:
进气畸变实验是航空发动机气动稳定性评定的重要方法之一。为克服传统设计方法逼近目标畸变图谱准确性低、实验迭代次数多等缺点,提出基于丝网间距和多孔介质映射关系,采用Fluent设计目标图谱畸变网的设计体系。设计了稳态总压测试系统,完成了畸变发生器的实物设计及风洞试验,畸变指数误差小于1.5%。试验结果表明设计体系可以高精度、高效地模拟畸变要求。
关键词:    航空发动机    畸变模拟网    Fluent    多孔介质模型    稳态总压测试系统   
A new intake distortion design system for research
CUI Jiahang1, LI Jianghong1, LI Xiaoyu2, DONG Suyan1, CAI Feichao1, FAN Wei1
1. School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China;
2. Chinese Flight Test Establishment, Xi'an 710089, China
Abstract:
The intake distortion experiment is one of the important methods for aero-engine aerodynamic stability assessment. In this paper, in order to overcome the shortcomings of traditional design methods such as low accuracy in approximating the target distortion map and many experimental iterations, a design system is proposed to design the target map distortion network using Fluent based on the mapping relationship between screen distance and porous media. Finally, the steady-state total pressure test system is designed, and the physical design of the distortion generator and wind tunnel test are completed, with the error of distortion index of less than 1.5%. The test results show that the design system can simulate the distortion requirements with high accuracy and efficiency.
Key words:    aero-engine    distortion simulation network    Fluent    porous medium model    steady-state total pressure test system   
收稿日期: 2022-06-09     修回日期:
DOI: 10.1051/jnwpu/20234120363
基金项目: 两机重大专项(J2019-I-0003-0004)资助
通讯作者: 李江红(1970-),西北工业大学副教授,主要从事航空发动机气动稳定性研究。e-mail:jhli@nwpu.edu.cn     Email:jhli@nwpu.edu.cn
作者简介: 崔佳航(1998-),西北工业大学硕士研究生,主要从事航空发动机气动稳定性研究。
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参考文献:
[1] XU Wenfeng, Sun Peng, YANG Guogang, et al. Numerical research on inlet total pressure distortion in a transonic compressor with non-axisymmetric stator clearance[J]. Journal of Thermal Science, 2020, 29:893-905
[2] 侯敏杰, 叶巍, 彭生红. 关于未来进气道/发动机相容性技术的探讨[J]. 航空科学技术, 2012, 2(5):5-8 HOU Minjie, YE Wei, PENG Shenghong. Investigation on compatibility of future inlet/engine[J]. Aeronautical Science and Technology, 2012, 2(5):5-8 (in Chinese)
[3] 代冰, 叶巍. 美、俄航空发动机稳定性标准对比分析[J]. 航空标准化与质量, 2009, 21(2):44-48 DAI Bing, YE Wei. Comparison and analysis of aeroengine stability standards between the United States and Russia[J]. Aeronautic Standardization & Quality, 2009, 21(2):44-48 (in Chinese)
[4] 薛海波. 插板后畸变流场的数值模拟及参数分析[D]. 南京:南京航空航天大学, 2008 XUE Haibo. Numerical simulation and parametric analysis of the distorted flow field after inserting the plate[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2008 (in Chinese)
[5] 严伟. 航空发动机气动稳定性分析数学模型研究与应用[D]. 南京:南京航空航天大学, 2016 YAN Wei. Research and application of mathematic model for aerodynamic stability analysis on aviation engine[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2016 (in Chinese)
[6] 丁宁. 大涵道比涡扇发动机进气总压畸变模拟及稳定性计算分析[D]. 南京:南京航空航天大学, 2015 DING Ning. Inlet total pressure distortion modeling and stability analysis of high bypass ratio turbofan engine[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2015 (in Chinese)
[7] 李文兰, 黄智涛, 乔渭阳. 进气畸变模拟网的设计与试验验证[J]. 航空学报, 1994, 15(6):658-664 LI Wenlan, HUANG Zhitao, QIAO Weiyang. Design and validation of simulation screen for inlet flow distortion[J]. Acta Aeronauticaet Astronautica Sinica, 1994, 15(6):658-664 (in Chinese)
[8] BEALE D K, CRAMER K B, KINGKANA Dr P S. Development of improved methods for simulating aircraft inlet distortion in turbine engine ground tests[C]//22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2022
[9] FANG Boyang, QIANG Xiaoqing. Design of aircraft engine inlet radial distortion generator[C]//Proceedings of the International Conference on Aerospace System Science and Engineering, Singapore, 2021:175-186
[10] BERNHARD H Anderson, JAMES Gibb. Vortex-generator installation studies on steady-state and dynamic distortion[J]. Journal of Aircraft, 1998, 35(4):513-520
[11] 胡骏, 赵运生, 丁宁, 等. 进气畸变对大涵道比涡扇发动机稳定性的影响[J]. 航空发动机, 2013, 39(6):6-12 HU Jun, ZHAO Yunsheng, DING Ning, et al. Investigation of influence of inlet distortion on high bypass ratio turbofan engine stability[J]. Aeroengine, 2013, 39(6):6-12 (in Chinese)
[12] 张生, 任文成, 屠宝锋, 等. 畸变网CFD数值模拟研究[J]. 沈阳航空航天大学学报, 2013, 30(5):27-32 ZHANG Sheng, REN Wencheng, TU Baofeng, et al. CFD numerical simulating investigation on distortion net[J]. Journal of Shenyang Aerospace University, 2013, 30(5):27-32 (in Chinese)
[13] 朱旭东. 湍流模型的比较、改进和应用[D]. 南京:南京航空航天大学, 2005 ZHU Xudong. Comparison, improvement and application of turbulence models[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2005 (in Chinese)
[14] 步娟娟. 多孔介质流动阻力及流动干扰影响研究[D]. 内蒙古:内蒙古科技大学, 2020 BU Juanjuan. Study on the flow resistance and interference of porous media[D]. Inner Mongolia:Inner Mongolia University of Science & Technology, 2020 (in Chinese)
[15] LEE K, LEE B, KANG S, et al. Inlet distortion test with gas turbine engine in the altitude engine test facility[C]//27th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Chicago, 2010