李白杨 , 祝小平 , 周洲 , 李明浩 , 王贵晨 , 王睿 . 串列翼布局分布式推进/气动耦合特性车载试验研究[J]. 航空学报, 0 : 1 -0 . DOI: 10.7527/S1000-6893.2026.32807

[1]黄俊.分布式电推进飞机设计技术综述[J].航空学报, 2021, 42(3):13-29
[2]HUANG J[J].Acta Aeronautica et Astronautica Sinica, 2021, 42(3): 13-29. (in Chinese).
[3]朱炳杰, 杨希祥, 宗建安, 等.分布式混合电推进飞行器技术[J].航空学报, 2022, 43(7):48-64
[4]ZHU B J, YANG X X, ZONG J A, et al.Review of distributed hybrid electric propulsion aircraft technolo-gy[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(7) (in Chinese)
[5]罗彧.2024年航空电推进系统进展[J]. 航空动力, 2025(1): 39-43.
[6]LUO Y.Progress of Aviation Electric Propulsion Sys-tem in 2024[J]. Aerospace Power, 2025(1): 39-43. (in Chinese)
[7]KIM H D, PERRY A T, ANSELL P J.A Review of Distributed Electric Propulsion Concepts for Air Vehicle Technology[C]//2018 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS). 2018: 1-21.
[8]HOOVER C B, SHEN J, KRESHOCK A R.Propeller Whirl Flutter Stability and Its Influence on X-57 Aircraft Design[J].Journal of Aircraft, 2018, 55(5):2169-2175
[9]庞圣钊, 刘恒, 王浩宇, 等.基于强化学习的分布式电推进飞机动力偏航控制[J/OL].推进技术, （2025-06-27）[2025-09-15].https://link.cnki.net/urlid/11.1813.v.20250627.0939.002.
[10]PANG S Z, LIU H, WANG H Y, et al.Power yaw con-trol for distributed electric propulsion aircraft based on reinforcement learning [J/OL]. Journal of Propul-sion Technology, （2025-06-27）[2025-09-15] .https://link.cnki.net/urlid/11.1813.v.20250627.0939.002.
[11]DEERE K A, VIKEN J K, VIKEN S, et al.Computa-tional Analysis of a Wing Designed for the X-57 Dis-tributed Electric Propulsion Aircraft[C]//35th AIAA Applied Aerodynamics Conference. Denver, Colora-do: American Institute of Aeronautics and Astro-nautics, 2017.
[12]贺之豪, 寇鹏, 梁博华, 等.考虑滑流效应的分布式电推进飞机动力偏航预测控制[J/OL].航空学报, （2025-06-23）[2025-09-15].https://link.cnki.net/urlid/11.1929.V.20250620.1658.012.
[13]HE Z H, KOU P, LIANG B H, et al.Powered yaw predictive control of distributed electric propulsion air-craft considering slipstream effects [J/OL]. Acta Aero-nautica et Astronautica Sinica, （2025-06-23）[2025-09-15]. https://link.cnki.net/urlid/11.1929.V.20250620.1658.012.
[14]郝智渊, 段辰龙, 宋万强, 等.分布式电推进飞机动力学特性分析与评估[J].飞行力学, 2023, 41(6):16-20
[15]HAO Z Y, DUAN C L, SONG W Q, et al.Analysis and evaluation for dynamics characteristics of distrib-uted electric propulsion aircraft[J].Flight Dynamics, 2023, 41(6):16-20
[16]REEL J L, BALTADJIEV N D.Using Computational Fluid Dynamics to Generate Complex Aerodynam-ic Database for VTOL Aircraft[C]//2018 Applied Aer-odynamics Conference. Atlanta, Georgia: American Institute of Aeronautics and Astronautics, 2018.
[17]王科雷, 周洲, 李明浩.动力翼单元松耦合设计方法研究及试验验证[J].航空学报, 2025, 46(9):218-235
[18]WANG K L， ZHOU Z， LI M H.Research and ex-perimental validation of loose coupling design method for propulsion wing unit[J].Acta Aeronautica et Astronautica Sinica, 2025, 46(9):131150-
[19]DE WAGTER C, REMES B, SMEUR E, et al.The NederDrone: A hybrid lift,hybrid energy hydrogen UAV[J].International Journal of Hydrogen Energy, 2021, 46(29):16003-16018
[20]SIMMONS B M.System Identification Approach for eVTOL Aircraft Demonstrated Using Simulated Flight Data[J].Journal of Aircraft, 2023, 60(4):1078-1093
[21]SIMMONS B M, MURPHY P C.Aero-Propulsive Modeling for Tilt-Wing,Distributed Propulsion Air-craft Using Wind Tunnel Data[J].Journal of Aircraft, 2022, 59(5):1162-1178
[22]ZHAO C, WANG D, YU T, et al.Direct Numerical Simulation of Tandem-Wing Aerodynamic Interac-tions at Low Reynolds Number[J].AIAA Journal, 2024, 62(12):4732-4750
[23]杨芃芊, 陈禹彤, 刘俊辉, 等.串列翼货运无人机大攻角气动与操稳特性[J].航空学报, 2025, 46(9):186-201
[24]YANG P Q, CHEN Y T, LIU J H, et al.Aerodynamic and operational characteristics analysis for tandem wing cargo UAV at high angle of attack[J].Acta Aero-nautica et Astronautica Sinica, 2025, 46(9):131056-
[25]JONES R, CLEAVER D J, GURSUL I.Aerodynam-ics of biplane and tandem wings at low Reynolds numbers[J].Experiments in Fluids, 2015, 56(6):124-
[26]张子军, 赵彤, 孙烨, 等.飞机大迎角飞行问题研究综述[J].航空工程进展, 2022, 13(3):74-85
[27]ZHANG Z J, ZHAO T, SUN Y, et al.Review of the Study on High-angle-of-attack Flight Problems of Aircraft[J].Advances in Aeronautical Science and Engineering, 2022, 13(3):74-85
[28]王科雷, 周洲, 郭佳豪, 等.分布式动力翼前飞状态动力气动耦合特性[J].航空学报, 2024, 45(2):137-155
[29]WANG K L, ZHOU Z, GUO J H, et al.Propul-siveaerodynamic coupled characteristics of distribut-ed-propulsion-wing during forward flight[J].Acta Aer-onautica et Astronautica Sinica, 2024, 45(2):128643-
[30]张卫国, 唐敏, 武杰, 等.倾转旋翼机风洞试验综述[J].航空学报, 2024, 45(9):29-58
[31]ZHANG W G， TANG M， WU J， et al.Over-view of wind tunnel test research on tiltrotor aircraft[J].Acta Aeronautica et Astronautica Sinica, 2024, 45(9):530114-
[32]PAPATHAKIS K V, KLOESEL K J, LIN Y, et al.NASA Turbo-electric Distributed Propulsion Bench[C]//52nd AIAA/SAE/ASEE Joint Propulsion Conference. Salt Lake City, UT: American Institute of Aeronautics and Astronautics, 2016.
[33]张星雨, 高正红, 雷涛, 等.分布式电推进飞机气动-推进耦合特性地面试验[J].航空学报, 2022, 43(8):406-416
[34]ZHANG X Y, GAO Z H, LEI T, et al.Ground test on aerodynamic-propulsion coupling characteristics of distributed electric propulsion aircraft[J].Acta Aero-nautica et Astronautica Sinica, 2022, 43(8):125389-
[35]赵清风, 周洲, 李明浩, 等.分布式动力翼-诱导翼面推进-气动耦合模型[J].航空学报, 2024, 45(10):150-164
[36]ZHAO Q F, ZHOU Z, LI M H, et al.Propul-sionaerodynamic coupling modeling for distributed-propulsion-wing with induced wing configuration[J].Acta Aeronautica et Astronautica Sini-ca, 2024, 45(10):129252-
[37]孙蓬勃, 周洲, 李旭, 等.目标气动特性下动力翼参数影响分析与优化[J].航空学报, 2024, 45(6):204-221
[38]SUN P B, ZHOU Z, LI X, et al.Influence analysis and optimization of distribution-propulsion-wing parame-ters with target aerodynamic characteristics[J].Acta Aeronautica et Astronautica Sini-ca, 2024, 45(6):629368-