| Citation: | WANG Yining, JI Jiayuan, ZHANG Xintao, et al. CFD-based research on exhaust characteristics of ejector for a propfan engine nacelle ventilating[J]. Journal of Aerospace Power, 2026, 41（5）：20240555 doi: 10.13224/j.cnki.jasp.20240555
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In order to analyze the influence of ejection ventilation structure on exhaust flow performance under low altitude and low speed conditions of a propfan engine configuration, a simulation model incorporating core compartment/internal nozzle/ejection outlet was constructed. The influences of various ejection structure schemes on exhaust characteristics were researched by numerical simulation method, and the causes for the change were analyzed from the perspective of flow mechanism. The results showed that the secondary flow coefficient decreased with the increase of the length ratio of the ejector outlet under low-altitude and low-speed conditions, and the trend was gentle later, simultaneously the peak appeared near a certain value with the decrease of the opening ratio
| [1] |
黄兴, 李伟, 杨宇飞, 等. 桨扇发动机推进效率分析方法研究[J]. 航空工程进展, 2024, 15(4): 50-55. HUANG Xing, LI Wei, YANG Yufei, et al. Research on analysis method of propulsive efficiency of prop-fan engine[J]. Advances in Aeronautical Science and Engineering, 2024, 15(4): 50-55. (in Chinese
HUANG Xing, LI Wei, YANG Yufei, et al. Research on analysis method of propulsive efficiency of prop-fan engine[J]. Advances in Aeronautical Science and Engineering, 2024, 15(4): 50-55. (in Chinese)
|
| [2] |
周莉, 是介, 王占学. 开式转子发动机研究进展[J]. 推进技术, 2019, 40(9): 1921-1932. ZHOU Li, SHI Jie, WANG Zhanxue. Research progress in open rotor engine[J]. Journal of Propulsion Technology, 2019, 40(9): 1921-1932. (in Chinese
ZHOU Li, SHI Jie, WANG Zhanxue. Research progress in open rotor engine[J]. Journal of Propulsion Technology, 2019, 40(9): 1921-1932. (in Chinese)
|
| [3] |
PAN Chengxiong, ZHANG Jingzhou, SHAN Yong. Effects of exhaust temperature on helicopter infrared signature[J]. Applied Thermal Engineering, 2013, 51(1/2): 529-538. doi: 10.1016/j.applthermaleng.2012.09.016
|
| [4] |
PAN Chengxiong, ZHANG Jingzhou, REN Lifeng, et al. Effects of rotor downwash on exhaust plume flow and helicopter infrared signature[J]. Applied Thermal Engineering, 2014, 65(1/2): 135-149. doi: 10.1016/j.applthermaleng.2014.01.009
|
| [5] |
张志伟, 马松, 陈雪芳, 等. 收敛喷管的引射效应对背负式短舱温度影响研究[J]. 飞机设计, 2014, 34(6): 1-6. ZHANG Zhiwei, MA Song, CHEN Xuefang, et al. Research on the influence of convergent nozzle ejector effect on top-mounted nacelle of the temperature field[J]. Aircraft Design, 2014, 34(6): 1-6. (in Chinese
ZHANG Zhiwei, MA Song, CHEN Xuefang, et al. Research on the influence of convergent nozzle ejector effect on top-mounted nacelle of the temperature field[J]. Aircraft Design, 2014, 34(6): 1-6. (in Chinese)
|
| [6] |
ZHANG Jingyang, GENG Jinxin, YANG Sen, et al. Influence of geometric parameters on the performance of ejector used in aeroengine air system[J]. Thermal Science and Engineering Progress, 2023, 37: 101571. doi: 10.1016/j.tsep.2022.101571
|
| [7] |
王广振, 吴寿生, 王之珊, 等. 混合管面积和位置对排气引射器性能的影响[J]. 推进技术, 2000, 21(4): 20-23. WANG Guangzhen, WU Shousheng, WANG Zhishan, et al. Effect of mixing tube area and position on performances for lobed ejector[J]. Journal of Propulsion Technology, 2000, 21(4): 20-23. (in Chinese
WANG Guangzhen, WU Shousheng, WANG Zhishan, et al. Effect of mixing tube area and position on performances for lobed ejector[J]. Journal of Propulsion Technology, 2000, 21(4): 20-23. (in Chinese)
|
| [8] |
饶珠明, 王兵. 微型涡喷发动机引射特性研究[J]. 弹箭与制导学报, 2017, 37(4): 106-108, 127. RAO Zhuming, WANG Bing. Study on ejection performance of micro-turbojet engine[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017, 37(4): 106-108, 127. (in Chinese doi: 10.15892/j.cnki.djzdxb.2017.04.025
RAO Zhuming, WANG Bing. Study on ejection performance of micro-turbojet engine[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017, 37(4): 106-108, 127. (in Chinese) doi: 10.15892/j.cnki.djzdxb.2017.04.025
|
| [9] |
叶宇琛. 直升机排气引射器配合角度对引射性能的影响[J]. 中国科技信息, 2020(6): 24-27. YE Yuchen. Influence of matching angle of helicopter exhaust ejector on ejector performance[J]. China Science and Technology Information, 2020(6): 24-27. (in Chinese doi: 10.3969/j.issn.1001-8972.2020.06.005
YE Yuchen. Influence of matching angle of helicopter exhaust ejector on ejector performance[J]. China Science and Technology Information, 2020(6): 24-27. (in Chinese) doi: 10.3969/j.issn.1001-8972.2020.06.005
|
| [10] |
钱尧一, 侯亮, 卜祥建, 等. 发动机舱排气引射系统多目标优化设计[J]. 工程机械, 2014, 45(1): 40-45, 120. QIAN Yaoyi, HOU Liang, BU Xiangjian, et al. Multi-objective optimal design of underhood exhaust ejector system in engine compartment[J]. Construction Machinery and Equipment, 2014, 45(1): 40-45, 120. (in Chinese
QIAN Yaoyi, HOU Liang, BU Xiangjian, et al. Multi-objective optimal design of underhood exhaust ejector system in engine compartment[J]. Construction Machinery and Equipment, 2014, 45(1): 40-45, 120. (in Chinese)
|
| [11] |
马帅, 王晓雨. 引射器数值模拟与关键结构参数优化设计[J]. 机械工程与自动化, 2024, 53(4): 55-57. MA Shuai, WANG Xiaoyu. Numerical simulation and key structural parameter optimization design of ejector[J]. Mechanical Engineering & Automation, 2024, 53(4): 55-57. (in Chinese doi: 10.3969/j.issn.1672-6413.2024.04.019
MA Shuai, WANG Xiaoyu. Numerical simulation and key structural parameter optimization design of ejector[J]. Mechanical Engineering & Automation, 2024, 53(4): 55-57. (in Chinese) doi: 10.3969/j.issn.1672-6413.2024.04.019
|
| [12] |
骆广琦, 李游, 刘琨, 等. 变循环发动机组合变几何调节方案[J]. 航空动力学报, 2014, 29(10): 2273-2278. LUO Guangqi, LI You, LIU Kun, et al. Combined variable geometry regulation schemes for variable cycle engine[J]. Journal of Aerospace Power, 2014, 29(10): 2273-2278. (in Chinese doi: 10.13224/j.cnki.jasp.2014.10.001
LUO Guangqi, LI You, LIU Kun, et al. Combined variable geometry regulation schemes for variable cycle engine[J]. Journal of Aerospace Power, 2014, 29(10): 2273-2278. (in Chinese) doi: 10.13224/j.cnki.jasp.2014.10.001
|
| [13] |
窦健, 吴琼. 变循环发动机后涵道引射器调节工况的数值研究[J]. 机械制造与自动化, 2020, 49(3): 195-197. DOU Jian, WU Qiong. Research on operating characteristics of rear variable area bypass circular injector of variable cycle engine[J]. Machine Building & Automation, 2020, 49(3): 195-197. (in Chinese doi: 10.19344/j.cnki.issn1671-5276.2020.03.052
DOU Jian, WU Qiong. Research on operating characteristics of rear variable area bypass circular injector of variable cycle engine[J]. Machine Building & Automation, 2020, 49(3): 195-197. (in Chinese) doi: 10.19344/j.cnki.issn1671-5276.2020.03.052
|
| [14] |
窦健, 汪明生, 吴琼. 变循环发动机后可变面积环形涵道引射器工作特性研究[C]//第八届中国航空学会青年科技论坛论文集. 广东 江门: 中国航空学会, 2018: 168-174. DOU Jian, WANG Mingsheng, WU Qiong. Research on operating characteristics of rear variable bypass circular injector of variable cyc engine[C]//8th Youth Technology 8th Youth Technology Conference of Chinese Aerospace Society Arcticles Collection. Jiangmen Guangdong: Chinese Aerospace Society, 2018: 168-174. (in Chinese
DOU Jian, WANG Mingsheng, WU Qiong. Research on operating characteristics of rear variable bypass circular injector of variable cyc engine[C]//8th Youth Technology 8th Youth Technology Conference of Chinese Aerospace Society Arcticles Collection. Jiangmen Guangdong: Chinese Aerospace Society, 2018: 168-174. (in Chinese)
|
| [15] |
LINEBERRY D, LANDRUM B. Effects of multiple nozzles on asymmetric ejector performance[R]. AIAA-2005-4283, 2005.
|
| [16] |
LIU Huadong, DANG Hao, JIN Zhaoyang, et al. Effects of the nozzle throat diameter on a bi-evaporator compression/ejection refrigeration system[J]. Heat and Mass Transfer, 2022, 58(12): 2207-2219. doi: 10.1007/s00231-022-03205-2
|
| [17] |
袁建新, 余建祖, 王先炜, 等. 基于旋翼下洗流场的直升机动力舱通风冷却系统仿真[J]. 直升机技术, 2009(1): 31-36. YUAN Jianxin, YU Jianzu, WANG Xianwei, et al. Simulation study of helicopter nacelle ventilation cooling system considering of downwash flow[J]. Helicopter Technique, 2009(1): 31-36. (in Chinese doi: 10.3969/j.issn.1673-1220.2009.01.007
YUAN Jianxin, YU Jianzu, WANG Xianwei, et al. Simulation study of helicopter nacelle ventilation cooling system considering of downwash flow[J]. Helicopter Technique, 2009(1): 31-36. (in Chinese) doi: 10.3969/j.issn.1673-1220.2009.01.007
|
| [18] |
张镜洋, 吴聪慧, 成锋娜, 等. 流动参数对发动机冷却用引射器性能的影响[J]. 航空动力学报, 2021, 36(5): 977-986. ZHANG Jingyang, WU Conghui, CHENG Fengna, et al. Effect of flow parameters on ejection performance of ejector for engine cooling[J]. Journal of Aerospace Power, 2021, 36(5): 977-986. (in Chinese doi: 10.13224/j.cnki.jasp.2021.05.009
ZHANG Jingyang, WU Conghui, CHENG Fengna, et al. Effect of flow parameters on ejection performance of ejector for engine cooling[J]. Journal of Aerospace Power, 2021, 36(5): 977-986. (in Chinese) doi: 10.13224/j.cnki.jasp.2021.05.009
|
| [19] |
孙顺利, 李纲, 芦海洋, 等. 主动引射自由射流试验系统舱压的仿真建模分析[J]. 推进技术, 2022, 43(5): 200994. SUN Shunli, LI Gang, LU Haiyang, et al. Modeling analysis on vacuum pressure of a free jet test system with active ejector[J]. Journal of Propulsion Technology, 2022, 43(5): 200994. (in Chinese doi: 10.13675/j.cnki.tjjs.200994
SUN Shunli, LI Gang, LU Haiyang, et al. Modeling analysis on vacuum pressure of a free jet test system with active ejector[J]. Journal of Propulsion Technology, 2022, 43(5): 200994. (in Chinese) doi: 10.13675/j.cnki.tjjs.200994
|
| [20] |
CONNER D, EDWARDS B, KLEIN P, et al. NASA/Army/Bell XV-15 tiltrotor low noise terminal area operations flight research program[R]. AIAA-2000-1923, 2000.
|
| [21] |
TAI T. Simulation and analysis of V-22 tiltrotor aircraft forward flight flowfield[R]. AIAA-1995-45, 1995.
|
| [22] |
陈尧, 单勇, 张靖周. 涡桨发动机舱引射通风冷却数值研究[J]. 航空计算技术, 2024, 54(1): 76-81. CHEN Yao, SHAN Yong, ZHANG Jingzhou. Numerical study on exhaust ejection and nacelle cooling of turboprop engine[J]. Aeronautical Computing Technique, 2024, 54(1): 76-81. (in Chinese
CHEN Yao, SHAN Yong, ZHANG Jingzhou. Numerical study on exhaust ejection and nacelle cooling of turboprop engine[J]. Aeronautical Computing Technique, 2024, 54(1): 76-81. (in Chinese)
|
| [23] |
DEWEY P E, VICK A R. An investigation of the discharge and drag characteristics of auxiliary-air outlets discharging into a transonic stream[R]. NACA-TN-3466, 1955.
|
| [24] |
环夏, 杨青真, 高翔, 等. 大涵道比涡扇发动机分开式排气系统设计参数影响研究[J]. 航空工程进展, 2013, 4(2): 211-218. HUAN Xia, YANG Qingzhen, GAO Xiang, et al. Numerical investigation into the effect of design parameters on high bypass ratio separate flow exhaust system performance[J]. Advances in Aeronautical Science and Engineering, 2013, 4(2): 211-218. (in Chinese doi: 10.3969/j.issn.1674-8190.2013.02.013
HUAN Xia, YANG Qingzhen, GAO Xiang, et al. Numerical investigation into the effect of design parameters on high bypass ratio separate flow exhaust system performance[J]. Advances in Aeronautical Science and Engineering, 2013, 4(2): 211-218. (in Chinese) doi: 10.3969/j.issn.1674-8190.2013.02.013
|
| [25] |
陈灿平, 李漫露, 田晓沛. 分开式排气系统气动性能与喷流特性数值研究[J]. 航空发动机, 2017, 43(2): 23-30. CHEN Canping, LI Manlu, TIAN Xiaopei. CFD-based research on aerodynamic performance of separate-flow exhaust system of high bypass ratio turbofan engine[J]. Aeroengine, 2017, 43(2): 23-30. (in Chinese doi: 10.13477/j.cnki.aeroengine.2017.02.005
CHEN Canping, LI Manlu, TIAN Xiaopei. CFD-based research on aerodynamic performance of separate-flow exhaust system of high bypass ratio turbofan engine[J]. Aeroengine, 2017, 43(2): 23-30. (in Chinese) doi: 10.13477/j.cnki.aeroengine.2017.02.005
|
| [26] |
邓文剑, 代瑛, 王家启. 引射喷管流量及推力特性数值研究[J]. 航空科学技术, 2014, 25(6): 9-13. DENG Wenjian, DAI Ying, WANG Jiaqi. Numerical investigation on mass-flow and thrust performance of the ejector-nozzle[J]. Aeronautical Science & Technology, 2014, 25(6): 9-13. (in Chinese
DENG Wenjian, DAI Ying, WANG Jiaqi. Numerical investigation on mass-flow and thrust performance of the ejector-nozzle[J]. Aeronautical Science & Technology, 2014, 25(6): 9-13. (in Chinese)
|
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