| Citation: | ZHOU Haoyu, WU Zhenlong, XIE Maixiang, et al. Numerical simulation on bird ingestion characteristics from engine inlet of turboprop aircraft[J]. Journal of Aerospace Power, 2024, 39（12）：20230083 doi: 10.13224/j.cnki.jasp.20230083
|
According to airworthiness regulations, attribute analysis on common foreign objects—birds, was conducted, and their geometric, mass, initial attitude, and velocity characteristics were determined; through computational fluid dynamics (CFD), the “dynamic grid method” and the six degrees of freedom method were coupled to numerically simulate the bird swallowing characteristics of the main engine inlet of a turboprop aircraft. The influence of the trajectory characteristics and exclusion characteristics of birds being sucked into the engine inlet was studied under the condition of integrated propeller/inlet/bypass channels. The results showed that the flow environment of the inlet may deteriorate, the total pressure coefficient of restitution in the aerodynamic interface plane (AIP) of the inlet may decrease, and the total pressure distortion may increase after the birds enter the inlet; under the simulated working conditions, birds were excluded from the side channel or collided with the wall of the side channel, which can be considered exclusion; the incoming Mach number had a significant impact on the attitude of birds before entering the inlet. At high outlet Mach numbers and high angles of attack, the bird body was more likely to be sucked into the main engine, which may have a serious impact on the main engine.
| [1] |
陈怀荣,王曦. 国外涡桨发动机控制技术的发展[J]. 航空发动机,2016,42(6): 9-17. CHEN Huairong,WANG Xi. Development of turboprop engine control technology in the west[J]. Aeroengine,2016,42(6): 9-17. (in Chinese
CHEN Huairong, WANG Xi. Development of turboprop engine control technology in the west[J]. Aeroengine, 2016, 42(6): 9-17. (in Chinese)
|
| [2] |
刘沛清. 空气螺旋桨理论及其应用[M]. 北京: 北京航空航天大学出版社,2006. LIU Peiqing. Air propeller theory and its application[M]. Beijing: Beijing University of Aeronautics and Astronautics Press,2006. (in Chinese
LIU Peiqing. Air propeller theory and its application[M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2006. (in Chinese)
|
| [3] |
李杰,杨钊,段卓毅,等. 涡桨飞机发展现状及关键气动问题[J]. 航空学报,2019,40(4): 71-81. LI Jie,YANG Zhao,DUAN Zhuoyi,et al. Development status and key aerodynamic problems of turboprop aircraft[J]. Acta Aeronautica et Astronautica Sinica,2019,40(4): 71-81. (in Chinese
LI Jie, YANG Zhao, DUAN Zhuoyi, et al. Development status and key aerodynamic problems of turboprop aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2019, 40(4): 71-81. (in Chinese)
|
| [4] |
陈佳慧,胡宇群,陈川. 大型民用飞机风挡鸟撞的适航分析与数值仿真[J]. 航空计算技术,2016,46(4): 91-94,98. CHEN Jiahui,HU Yuqun,CHEN Chuan. Airworthiness analysis and numerical simulation of bird impact on large civil aircraft windshield[J]. Aeronautical Computing Technique,2016,46(4): 91-94,98. (in Chinese doi: 10.3969/j.issn.1671-654X.2016.04.023
CHEN Jiahui, HU Yuqun, CHEN Chuan. Airworthiness analysis and numerical simulation of bird impact on large civil aircraft windshield[J]. Aeronautical Computing Technique, 2016, 46(4): 91-94, 98. (in Chinese) doi: 10.3969/j.issn.1671-654X.2016.04.023
|
| [5] |
付焱晶. 直升机发动机进气防护装置研究[D]. 沈阳: 东北大学,2011. FU Yanjing. Study on inlet protective equipment of helicopter engine[D]. Shenyang: Northeastern University,2011. (in Chinese
FU Yanjing. Study on inlet protective equipment of helicopter engine[D]. Shenyang: Northeastern University, 2011. (in Chinese)
|
| [6] |
陈晓,李潞龙,马若龙. 带有腔室旁通道的进气道气动性能试验研究[J]. 航空动力学报,1994,9(3): 42-45,107-108. CHEN Xiao,LI Lulong,MA Ruolong. Experimental study on aerodynamic performance of inlet with bypass channel[J]. Journal of Aerospace Power,1994,9(3): 42-45,107-108. (in Chinese
CHEN Xiao, LI Lulong, MA Ruolong. Experimental study on aerodynamic performance of inlet with bypass channel[J]. Journal of Aerospace Power, 1994, 9(3): 42-45, 107-108. (in Chinese)
|
| [7] |
徐弘历. 涡桨飞机进气道设计方法及性能研究[D]. 南京: 南京航空航天大学,2015. XU Hongli. Study on design method and performance of turboprop aircraft inlet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2015. (in Chinese
XU Hongli. Study on design method and performance of turboprop aircraft inlet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015. (in Chinese)
|
| [8] |
MI Baigang. A CFD-CSD coupling method for simulating the dynamic impact and expulsion of fragile foreign objects from the ‘inlet-bypass duct’ junction of a turboprop aircraft[J]. Engineering Applications of Computational Fluid Mechanics,2022,16(1): 73-94. doi: 10.1080/19942060.2021.2005684
|
| [9] |
PAPADAKIS M,YEONG H W,SUARES I,et al. Experimental and computational investigation of ice shedding from aircraft surfaces[R]. AIAA 2006-1010,2006.
|
| [10] |
BARUZZI G S,LAGACÉ P,AUBÉ M S,et al. Development of a shed-ice trajectory simulation in FENSAP-ICE[R]. Warrendale,PA,US: SAE Technical Paper Series 400 Commonwealth Drive,2007.
|
| [11] |
DESCHENES J M,BARUZZI G S,LAGACE P,et al. FENSAP-ICE: a CFD Monte Carlo approach to shed-ice trajectory and impact[R]. SAE Technical Paper 2011-38-0089,2011.
|
| [12] |
李玉龙,石霄鹏. 民用飞机鸟撞研究现状[J]. 航空学报,2012,33(2): 189-198. LI Yulong,SHI Xiaopeng. Investigation of the present status of research on bird impacting on commercial airplanes[J]. Acta Aeronautica et Astronautica Sinica,2012,33(2): 189-198. (in Chinese
LI Yulong, SHI Xiaopeng. Investigation of the present status of research on bird impacting on commercial airplanes[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(2): 189-198. (in Chinese)
|
| [13] |
MI Baigang,ZHAN Hao. Numerical simulation on rigid foreign object exclusion in the turboprop engine intake system with a bypass duct[J]. IEEE Access,1920,7: 61920-61933.
|
| [14] |
王利敏,张彦军,米百刚,等. 涡桨飞机发动机进气道排除异物特性数值研究[J]. 航空工程进展,2020,11(2): 264-271,278. WANG Limin,ZHANG Yanjun,MI Baigang,et al. Numerical simulation on excluding foreign objects from engine inlet of turboprop aircraft[J]. Advances in Aeronautical Science and Engineering,2020,11(2): 264-271,278. (in Chinese
WANG Limin, ZHANG Yanjun, MI Baigang, et al. Numerical simulation on excluding foreign objects from engine inlet of turboprop aircraft[J]. Advances in Aeronautical Science and Engineering, 2020, 11(2): 264-271, 278. (in Chinese)
|
| [15] |
李旦,赵廷渝,王永虎. 鸟撞飞机风挡数值模拟研究[J]. 四川理工学院学报(自然科学版),2017,30(4): 36-40. LI Dan,ZHAO Tingyu,WANG Yonghu. Numerical simulation of bird impact on aircraft windshield[J]. Journal of Sichuan University of Science & Engineering (Natural Science Edition),2017,30(4): 36-40. (in Chinese
LI Dan, ZHAO Tingyu, WANG Yonghu. Numerical simulation of bird impact on aircraft windshield[J]. Journal of Sichuan University of Science & Engineering (Natural Science Edition), 2017, 30(4): 36-40. (in Chinese)
|
| [16] |
唐伟,刘启国,朱瑾,等. FAR 33 与 GJB 241A 技术要求对比分析[J]. 航空标准化与质量,2012(4): 36-40. TANG Wei,LIU Qiguo,ZHU Jin,et al. Comparative analysis on technical requirements of FAR 33 and GJB 241A[J]. Aeronautic Standardization and Quality,2012(4): 36-40. (in Chinese
TANG Wei, LIU Qiguo, ZHU Jin, et al. Comparative analysis on technical requirements of FAR 33 and GJB 241A[J]. Aeronautic Standardization and Quality, 2012(4): 36-40. (in Chinese)
|
| [17] |
徐静,杨永,左岁寒. 模拟螺旋桨滑流的桨盘理论应用研究及验证[J]. 航空计算技术,2008,38(3): 65-67. XU Jing,YANG Yong,ZUO Suihan. Numerical simulation of propeller/wing-nacelle configuration interaction[J]. Aeronautical Computing Technique,2008,38(3): 65-67. (in Chinese doi: 10.3969/j.issn.1671-654X.2008.03.018
XU Jing, YANG Yong, ZUO Suihan. Numerical simulation of propeller/wing-nacelle configuration interaction[J]. Aeronautical Computing Technique, 2008, 38(3): 65-67. (in Chinese) doi: 10.3969/j.issn.1671-654X.2008.03.018
|
| [18] |
YAZAR I,YASA T,KIYAK E. Simulation-based steady-state aero-thermal model for small-scale turboprop engine[J]. Aircraft Engineering and Aerospace Technology,2017,89(2): 203-210. doi: 10.1108/AEAT-02-2015-0062
|
| [19] |
周诗睿. 螺旋桨与进气道的气动干扰研究[D]. 南京: 南京航空航天大学,2019. ZHOU Shirui. Research on aerodynamic interference of propeller and inlet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2019. (in Chinese
ZHOU Shirui. Research on aerodynamic interference of propeller and inlet[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019. (in Chinese)
|
| [20] |
RUIZ-CALAVERA L,FUNES-SEBASTIAN D,PERDONES-DIAZ D. Powered model wind tunnel tests of a high-offset subsonic turboprop air intake[R]. AIAA 2010-6502,2010.
|
| [21] |
CHEN Xi,HUTCHINSON J W. Particle impact on metal substrates with application to foreign object damage to aircraft engines[J]. Journal of the Mechanics and Physics of Solids,2002,50(12): 2669-2690. doi: 10.1016/S0022-5096(02)00022-4
|
| [22] |
MURMAN S,AFTOSMIS M,BERGER M. Simulations of 6-DOF motion with a Cartesian method[R]. AIAA 2003-1246,2003.
|
DownLoad:
