| Citation: | REN Jiahao, WU Zhenlong, TAN Huijun, et al. Coupled flow characteristic of inlet and tail-mounted propeller in tail-propelled unmanned aerial[J]. Journal of Aerospace Power, 2026, 41（6）：20250205 doi: 10.13224/j.cnki.jasp.20250205
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The coupled flow between an inlet and a tail-mounted propeller in unmanned aerial vehicles was examined using unsteady simulations with a sliding mesh technique. The influence of propeller rotation on the inlet flow field was analyzed in ground and cruise states. An integrated model of the airframe, inlet, and five-blade propeller was established with a hybrid hexahedral/polyhedral mesh. Results showed that in ground state, the propeller slipstream increased the total pressure recovery coefficient by 0.17% due to flow twisting and contraction, while the total pressure distortion index
| [1] |
郑伟连. 无人机动力进排气系统隐身设计分析[J]. 航空动力, 2019(4): 28-31. ZHENG Weilian. Analysis of stealth design for UAV inlet and exhaust systems[J]. Aerospace Power, 2019(4): 28-31. (in Chinese
ZHENG Weilian. Analysis of stealth design for UAV inlet and exhaust systems[J]. Aerospace Power, 2019(4): 28-31. (in Chinese)
|
| [2] |
郑高杰, 何小明, 李东坡, 等. 尾部推进无人机双90°偏折进气道/蜗壳耦合流动特性[J]. 航空学报, 2024, 45(4): 128782. ZHENG Gaojie, HE Xiaoming, LI Dongpo, et al. Double 90° deflection inlet/volute coupling flow characteristics of tail-powered unmanned aerial vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128782. (in Chinese doi: 10.7527/S1000-6893.2023.28782
ZHENG Gaojie, HE Xiaoming, LI Dongpo, et al. Double 90° deflection inlet/volute coupling flow characteristics of tail-powered unmanned aerial vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(4): 128782. (in Chinese) doi: 10.7527/S1000-6893.2023.28782
|
| [3] |
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)
|
| [4] |
周辉华. 国外涡桨发动机的发展[J]. 航空科学技术, 2013, 24(1): 18-22. ZHOU Huihua. The development prospect of turbo-propeller engines[J]. Aeronautical Science & Technology, 2013, 24(1): 18-22. (in Chinese doi: 10.13477/j.cnki.aeroengine.2016.06.002
ZHOU Huihua. The development prospect of turbo-propeller engines[J]. Aeronautical Science & Technology, 2013, 24(1): 18-22. (in Chinese) doi: 10.13477/j.cnki.aeroengine.2016.06.002
|
| [5] |
HAGER R D, VRABEL D. Advanced turboprop project[M]. Washington DC: Scientific and Technical Information Division, National Aeronautics and Space Administration, 1988.
|
| [6] |
罗天一, 单鹏, 孟斐, 等. 螺旋桨-自由涡轮涡桨发动机稳态/过渡态数值模拟[J]. 航空动力学报, 2017, 32(5): 1176-1182. LUO Tianyi, SHAN Peng, MENG Fei, et al. Steady-and transient-state numerical simulation of turboprop engine of propeller-free-turbine types[J]. Journal of Aerospace Power, 2017, 32(5): 1176-1182. (in Chinese doi: 10.13224/j.cnki.jasp.2017.05.019
LUO Tianyi, SHAN Peng, MENG Fei, et al. Steady-and transient-state numerical simulation of turboprop engine of propeller-free-turbine types[J]. Journal of Aerospace Power, 2017, 32(5): 1176-1182. (in Chinese) doi: 10.13224/j.cnki.jasp.2017.05.019
|
| [7] |
麻蓉, 高飞飞, 颜洪, 等. 螺旋桨飞机滑流非定常数值模拟研究[J]. 航空计算技术, 2016, 46(1): 27-30. MA Rong, GAO Feifei, YAN Hong, et al. Research on unsteady numerical simulation of propeller aircraft slipstream[J]. Aeronautical Computing Technique, 2016, 46(1): 27-30. (in Chinese
MA Rong, GAO Feifei, YAN Hong, et al. Research on unsteady numerical simulation of propeller aircraft slipstream[J]. Aeronautical Computing Technique, 2016, 46(1): 27-30. (in Chinese)
|
| [8] |
STUERMER A. Unsteady CFD simulations of propeller installation effects[R]. AIAA-2006-4969, 2006.
|
| [9] |
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.
|
| [10] |
YANG Yannian, ZHOU Teng, SCIACCHITANO A, et al. Propeller and inflow vortex interaction: vortex response and impact on the propeller performance[J]. CEAS Aeronautical Journal, 2016, 7(3): 419-428. doi: 10.1007/s13272-016-0198-z
|
| [11] |
FELLI M, CAMUSSI R, DI FELICE F. Mechanisms of evolution of the propeller wake in the transition and far fields[J]. Journal of Fluid Mechanics, 2011, 682: 5-53. doi: 10.1017/jfm.2011.150
|
| [12] |
PAKMEHR M, FITZGERALD N, FERON E, et al. Physics-based dynamic modeling of a turboshaft engine driving a variable pitch propeller[J]. Journal of Propulsion and Power, 2016, 32(3): 646-658. doi: 10.2514/1.B35163
|
| [13] |
ORTUN B, BOISARD R, GONZALEZ-MARTINO I. In-plane airloads of a propeller with inflow angle: prediction vs. experiment[R]. AIAA-2012-2778, 2012.
|
| [14] |
韦宇卿, 郭峰, 朱剑锋, 等. 前/后置螺旋桨对涡桨发动机性能影响的整机试验[J]. 航空动力学报, 2022, 37(1): 165-172. WEI Yuqing, GUO Feng, ZHU Jianfeng, et al. Experiment on influence of front/after-mounted propeller on turboprop engine performance[J]. Journal of Aerospace Power, 2022, 37(1): 165-172. (in Chinese doi: 10.13224/j.cnki.jasp.20210562
WEI Yuqing, GUO Feng, ZHU Jianfeng, et al. Experiment on influence of front/after-mounted propeller on turboprop engine performance[J]. Journal of Aerospace Power, 2022, 37(1): 165-172. (in Chinese) doi: 10.13224/j.cnki.jasp.20210562
|
| [15] |
陈荣钱, 王旭, 尤延铖. 短舱对螺旋桨滑流影响的IDDES数值模拟[J]. 航空学报, 2016, 37(6): 1851-1860. CHEN Rongqian, WANG Xu, YOU Yancheng. Numerical simulation of nacelle’s effects on propeller slipstream based on IDDES model[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(6): 1851-1860. (in Chinese doi: 10.7527/S1000-6893.2015.0353
CHEN Rongqian, WANG Xu, YOU Yancheng. Numerical simulation of nacelle’s effects on propeller slipstream based on IDDES model[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(6): 1851-1860. (in Chinese) doi: 10.7527/S1000-6893.2015.0353
|
| [16] |
王伟杰, 张宜琳, 吴卓远. 螺旋桨滑流对涡轮螺旋桨进气道气动性能影响仿真研究[J]. 机械设计与制造工程, 2024, 53(11): 75-79. WANG Weijie, ZHANG Yilin, WU Zhuoyuan. Simulation on the influence of propeller slipstream on aerodynamic performance of turboprop inlet[J]. Machine Design and Manufacturing Engineering, 2024, 53(11): 75-79. (in Chinese doi: 10.3969/j.issn.2095-509X.2024.11.014
WANG Weijie, ZHANG Yilin, WU Zhuoyuan. Simulation on the influence of propeller slipstream on aerodynamic performance of turboprop inlet[J]. Machine Design and Manufacturing Engineering, 2024, 53(11): 75-79. (in Chinese) doi: 10.3969/j.issn.2095-509X.2024.11.014
|
| [17] |
曾平君, 孙姝, 黄河峡, 等. 直升机/粒子分离器一体化流场特性: 第一部分 前进比的影响[J]. 航空动力学报, 2014, 29(4): 858-866. ZENG Pingjun, SUN Shu, HUANG Hexiao, et al. Integrated flow field characteristics of helicopter/particle separator: Part 1 influence of advance ratio[J]. Jounal of Aerospace Power, 2014, 29(4): 858-866. (in Chinese
ZENG Pingjun, SUN Shu, HUANG Hexiao, et al. Integrated flow field characteristics of helicopter/particle separator: Part 1 influence of advance ratio[J]. Jounal of Aerospace Power, 2014, 29(4): 858-866. （in Chinese）
|
| [18] |
GOLDEN D, BARBER T, CHIN W. An axisymmetric nacelle and turboprop inlet analysis with flow-through and power simulation capabilities[R]. AIAA 1982-256, 1982.
|
| [19] |
CORCIONE S, CUSATI V, CILIBERTI D, et al. Experimental assessment of aero-propulsive effects on a large turboprop aircraft with rear-engine installation[J]. Aerospace, 2023, 10(1): 85. doi: 10.3390/aerospace10010085
|
| [20] |
吴裕平, 习娟, 范俊. 共轴刚性旋翼高速直升机配平及旋翼系统气动特性研究[J]. 直升机技术, 2018(2): 1-7. WU Yuping, XI Juan, FAN Jun. The trim and the rotor aerodynamic characteristics research of the coaxial-rotor high speed helicopter[J]. Helicopter Technique, 2018(2): 1-7. (in Chinese doi: 10.3969/j.issn.1673-1220.2018.02.001
WU Yuping, XI Juan, FAN Jun. The trim and the rotor aerodynamic characteristics research of the coaxial-rotor high speed helicopter[J]. Helicopter Technique, 2018(2): 1-7. (in Chinese) doi: 10.3969/j.issn.1673-1220.2018.02.001
|
| [21] |
车海峰, 叶靓, 邱福生, 等. 机身形状对共轴尾推螺旋桨气动干扰影响研究[J]. 气动研究与试验, 2023(6): 41-50. CHE Haifeng, YE Liang, QIU Fusheng, et al. Research on aerodynamic interference influence of airframe shape on coaxial tail propeller[J]. Aerodynamic Research & Experiment, 2023(6): 41-50. (in Chinese doi: 10.20118/j.issn2097-258X.2023.06.004
CHE Haifeng, YE Liang, QIU Fusheng, et al. Research on aerodynamic interference influence of airframe shape on coaxial tail propeller[J]. Aerodynamic Research & Experiment, 2023(6): 41-50. (in Chinese) doi: 10.20118/j.issn2097-258X.2023.06.004
|
| [22] |
杨成凤, 段卓毅, 张宏, 等. 螺旋桨滑流对环形进气道性能影响的数值仿真[J]. 计算机仿真, 2022, 39(6): 36-41, 52. YANG Chengfeng, DUAN Zhuoyi, ZHANG Hong, et al. Numerical simulation study on effects of propeller slipstream on aerodynamic characteristics of annular intet[J]. Computer Simulation, 2022, 39(6): 36-41, 52. (in Chinese doi: 10.3969/j.issn.1006-9348.2022.06.008
YANG Chengfeng, DUAN Zhuoyi, ZHANG Hong, et al. Numerical simulation study on effects of propeller slipstream on aerodynamic characteristics of annular intet[J]. Computer Simulation, 2022, 39(6): 36-41, 52. (in Chinese) doi: 10.3969/j.issn.1006-9348.2022.06.008
|
| [23] |
ZHENG Gaojie, WU Zhenlong, TAN Huijun, et al. Aerodynamic study of a bifurcated turboprop engine inlet with a propeller for flow at ground suction conditions[J]. Aerospace Science and Technology, 2024, 155: 109720. doi: 10.1016/j.ast.2024.109720
|
| [24] |
REN Jiahao, WU Zhenlong, TAN Huijun, et al. Experimental investigation of the aerodynamics of a UAV inlet with double 90° bends[J]. Aerospace Science and Technology, 2024, 154: 109502. doi: 10.1016/j.ast.2024.109502
|
| [25] |
REN Jiahao, WU Zhenlong, TAN Huijun, et al. Experimental study of the aerodynamic performance and flow characteristics of an integrated UAV inlet with double 90° bends[J]. Aerospace, 2024, 11(7): 593. doi: 10.3390/aerospace11070593
|
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