Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (5): 529644-529644.doi: 10.7527/S1000-6893.2023.29644
• Reviews • Previous Articles Next Articles
Guangjia LI, Hongbo WANG(), Kai ZHANG, Zhisheng YI
Received:
2023-09-25
Revised:
2023-09-28
Accepted:
2023-10-08
Online:
2024-03-15
Published:
2023-10-13
Contact:
Hongbo WANG
E-mail:whb0126@163.com
CLC Number:
Guangjia LI, Hongbo WANG, Kai ZHANG, Zhisheng YI. Lift enhancement and drag reduction technologies of solar powered unmanned aerial vehicles in near space: Review[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529644-529644.
1 | 李锋,白鹏. 飞行器低雷诺数空气动力学[M]. 北京:中国宇航出版社, 2017:10-13. |
LI F, BAI P. Aerodyanamics of aircraft at low Reynolds number[M]. Beijing: China Aerospace Press, 2017:10-13 (in Chinese). | |
2 | LISSAMAN P S. Low-Reynolds-number airfoils[J]. Annual Review of Fluid Mechanics, 1983, 15: 223-239. |
3 | 左伟. 低雷诺数下机翼气动特性研究及控制[D]. 南京: 南京航空航天大学, 2016: 12-40. |
ZUO W. Research and control of aerodynamic characteristics of wing at low Reynolds number[D].Nanjing: Nanjing University of Aeronautics and Astronautics, 2016: 12-40 (in Chinese) . | |
4 | MUELLER T J, BATILL S M. Experimental studies of separation on a two-dimensional airfoil at low Reynolds numbers[J]. AIAA Journal, 1982, 20(4): 457-463. |
5 | 白鹏, 崔尔杰, 李锋, 等. 对称翼型低雷诺数小攻角升力系数非线性现象研究[J]. 力学学报, 2006, 38(1): 1-8. |
BAI P, CUI E J, LI F, et al. Study of the nonlinear lift coefficient of the symmetrical airfoil at low Reynolds number near the 0° angle of attack[J]. Chinese Journal of Theoretical and Applied Mechanics, 2006, 38(1): 1-8 (in Chinese). | |
6 | 黄江涛, 刘刚, 高正红. 飞行器气动综合优化设计理论与方法[M]. 北京: 科学出版社, 2022: 58-164. |
HUANG J T, LIU G, GAO Z H. Theory and method of aerodynamic comprehensive optimization design of aircraft[M]. Beijing: Science Press, 2022: 58-164 (in Chinese). | |
7 | GOPALARATHNAM A, SELIG M. Low speed NLF airfoils -A case study in inverse airfoil design[C]∥ Proceedings of the 37th Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 1999. |
8 | 张维智, 贺德馨, 张兆顺. 低雷诺数高升力翼型的设计和实验研究[J]. 空气动力学学报, 1998, 16(3): 363-367. |
ZHANG W Z, HE D X, ZHANG Z S. The design and experiment study for a high airfoil at low Reynold numbers[J]. Acta Aerodynamica Sinica, 1998, 16(3): 363-367 (in Chinese). | |
9 | 孔繁美, 华俊, 向锦武, 等. 高升力与失速特性缓和的翼型设计研究[J]. 北京航空航天大学学报, 2002, 28(2): 235-237. |
KONG F M, HUA J, XIANG J W, et al. Design and research of high-lift mild-stall airfoils[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(2): 235-237 (in Chinese). | |
10 | 左林玄, 王晋军. 低雷诺数翼型的优化设计[J]. 兵工学报, 2009, 30(8): 1073-1077. |
ZUO L X, WANG J J. Airfoil design optimization at low Reynolds number[J]. Acta Armamentarii, 2009, 30(8): 1073-1077 (in Chinese). | |
11 | 张亚锋, 宋笔锋, 李占科. 高升力翼型的气动优化设计和实验研究[J]. 飞行力学, 2006, 24(4): 70-72. |
ZHANG Y F, SONG B F, LI Z K. Aerodynamic optimization design and experiment study for a high-lift airfoil[J]. Flight Dynamics, 2006, 24(4): 70-72 (in Chinese). | |
12 | 邓磊, 乔志德, 杨旭东, 等. 高升阻比自然层流翼型多点/多目标优化设计[J]. 空气动力学学报, 2011, 29(3): 330-335. |
DENG L, QIAO Z D, YANG X D, et al. Multi-point/objective optimization design of high lift-to-drag ratio for NLF airfoils[J]. Acta Aerodynamica Sinica, 2011, 29(3): 330-335 (in Chinese). | |
13 | 陈学孔, 郭正, 易凡, 等. 低雷诺数翼型的气动外形优化设计[J]. 空气动力学学报, 2014, 32(3): 300-307. |
CHEN X K, GUO Z, YI F, et al. Aerodynamic shape optimization and design of airfoils with low Reynolds number[J]. Acta Aerodynamica Sinica, 2014, 32(3): 300-307 (in Chinese). | |
14 | 李帝辰, 杨龙, 魏闯, 等. 低雷诺数翼型多点气动优化设计方法研究[J]. 航空科学技术, 2020, 31(12): 16-25. |
LI D C, YANG L, WEI C, et al. Study on multi-point aerodynamic optimization method of low Reynolds number airfoil[J]. Aeronautical Science & Technology, 2020, 31(12): 16-25 (in Chinese). | |
15 | SELIG M, MCGRANAHAN B. Wind tunnel aerodynamic tests of six airfoils for use on small wind turbines[C]∥ Proceedings of the 42nd AIAA Aerospace Sciences Meeting and Exhibit. Reston: AIAA, 2004. |
16 | PADULA S L, GUMBERT C R, LI W. Aerospace applications of optimization under uncertainty[J]. Optimization and Engineering, 2006, 7(3): 317-328. |
17 | 张庆, 薛榕融, 马浩统. 低雷诺数仿生分离流翼型气动特性初探[J]. 航空动力学报, 2022, 37(7): 1516-1527. |
ZHANG Q, XUE R R, MA H T. Preliminary study on aerodynamic characteristics of bionic separated flow airfoil with low Reynolds number[J]. Journal of Aerospace Power, 2022, 37(7): 1516-1527 (in Chinese). | |
18 | 张子良, 张明明. 仿生减阻翼型的气动性能[J]. 航空动力学报, 2021, 36(8): 1740-1748. |
ZHANG Z L, ZHANG M M. Aerodynamic performance for bionic drag-reducing airfoil[J]. Journal of Aerospace Power, 2021, 36(8): 1740-1748 (in Chinese). | |
19 | 关惠仁, 方斌, 刘文玺, 等. 低雷诺数下仿生翼型的动力特性数值模拟[J]. 舰船科学技术, 2022, 44(2): 18-23. |
GUAN H R, FANG B, LIU W X, et al. Numerical simulation research on dynamic characteristics of bionic airfoil under low Reynolds number[J]. Ship Science and Technology, 2022, 44(2): 18-23 (in Chinese). | |
20 | 陶真新, 李绍斌, 宋西镇. 低雷诺数下柔性翼型气动性能分析[J]. 力学与实践, 2017, 39(2): 145-151. |
TAO Z X, LI S B, SONG X Z. The aerodynamic performance of a flexible airfoil at low Reynolds number[J]. Mechanics in Engineering, 2017, 39(2): 145-151 (in Chinese). | |
21 | GIGUERE P, LEMAY J, DUMAS G. Gurney flap effects and scaling for low-speed airfoils[C]∥ Proceedings of the 13th Applied Aerodynamics Conference. Reston: AIAA, 1995. |
22 | STORMS B, JANG C. Lift enhancement of an airfoil using a Gurney flap and vortex generators[C]∥ Proceedings of the 31st Aerospace Sciences Meeting. Reston: AIAA, 1993. |
23 | BROWN L, FILIPPONE A. Aerofoil at low speeds with Gurney flaps[J]. The Aeronautical Journal, 2003, 107(1075): 539-546. |
24 | 崔钊, 李建波, 赵洪. 翼型加装格尼襟翼的低雷诺数气动特性实验研究[J]. 实验流体力学, 2013, 27(4): 1-6. |
CUI Z, LI J B, ZHAO H. Experimental study on aerodynamic characteristics of airfoil equipped with Gurney flaps at low Reynolds numbers[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(4): 1-6 (in Chinese). | |
25 | 李亚臣, 王晋军. GURNEYFLAP增升研究综述[J]. 航空学报, 2000, 21(4): 380-382. |
LI Y C, WANG J J. Summary of GURNEYFLAP Ascension research[J]. Acta Aeronautica et Astronautica Sinica, 2000, 21(4): 380-382 (in Chinese). | |
26 | 石文, 李广佳, 仪志胜, 等. 临近空间太阳能无人机应用现状与展望[J]. 空天技术, 2022(1): 83-90. |
SHI W, LI G J, YI Z S, et al. Current status and prospect of solar-powered unmanned aerial vehicle application in near space[J]. Aerospace Technology, 2022(1): 83-90 (in Chinese). | |
27 | 苑轩. 我国首款大型太阳能无人机完成两万米高空飞行[J]. 中国航天, 2017(7): 33. |
YUAN X. China’s first large-scale solar drone completed 20, 000 meters high altitude flight[J]. Aerospace China, 2017(7): 33 (in Chinese). | |
28 | 马东立, 张良, 杨穆清, 等. 超长航时太阳能无人机关键技术综述[J]. 航空学报, 2020, 41(3): 623418. |
MA D L, ZHANG L, YANG M Q, et al. Review of key technologies of ultra-long-endurance solar powered unmanned aerial vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(3): 623418 (in Chinese). | |
29 | 阙建锋, 王维军, 吴宇. 利于减少配平损失的太阳能飞机构型设计[J]. 北京航空航天大学学报, 2016, 42(7): 1479-1485. |
QUE J F, WANG W J, WU Y. Design of solar-powered aircraft configuration for reducing trim loss[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(7): 1479-1485 (in Chinese). | |
30 | 赵炜, 黄江流, 周洲, 等. 菱形翼布局太阳能无人机螺旋桨滑流影响研究[J]. 北京航空航天大学学报, 2020, 46(7): 1296-1306. |
ZHAO W, HUANG J L, ZHOU Z, et al. Effects of propeller slipstream on diamond joined-wing configuration solar-powered UAV[J]. Journal of Beijing University of Aeronautics and Astronautics, 2020, 46(7): 1296-1306 (in Chinese). | |
31 | SCHARPF D, MUELLER T. An experimental study of a closely coupled tandem wing configurationat low Reynolds numbers[C]∥ Proceedings of the Flight Simulation Technologies Conference and Exhibit. Reston: AIAA, 1990. |
32 | 李广佳, 李锋, 石文. 串置翼型数值模拟及气动特性分析[J]. 飞机设计, 2006, 26(1): 19-24. |
LI G J, LI F, SHI W. Numerical simulations of tandem-airfoil[J]. Aircraft Design, 2006, 26(1): 19-24 (in Chinese). | |
33 | 王红波, 祝小平, 周洲, 等. 太阳能无人机螺旋桨滑流气动特性分析[J]. 西北工业大学学报, 2015, 33(6): 913-920. |
WANG H B, ZHU X P, ZHOU Z, et al. Aerodynamic investigation on propeller slipstream flows for solar powered airplanes[J]. Journal of Northwestern Polytechnical University, 2015, 33(6): 913-920 (in Chinese). | |
34 | WU M J, SHI Z W, XIAO T H, et al. Energy optimization and investigation for Z-shaped Sun-tracking morphing-wing solar-powered UAV[J]. Aerospace Science and Technology, 2019, 91: 1-11. |
35 | 周伟, 马培洋, 郭正, 等. 基于翼尖链翼的组合固定翼无人机研究[J]. 航空学报, 2022, 43(9): 325946. |
ZHOU W, MA P Y, GUO Z, et al. Research on combined fixed-wing UAV based on wing tip chain wing[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(9): 325946 (in Chinese). | |
36 | KROO I. Propeller-wing integration for minimum induced loss[J]. Journal of Aircraft, 1986, 23(7): 561-565. |
37 | RAKSHITH B R, DESHPANDE S M, NARASIMHA R, et al. Optimal low-drag wing planforms for tractor-configuration propeller-driven aircraft[J]. Journal of Aircraft, 2015, 52(6): 1791-1801. |
38 | BORER N K, PATTERSON M D, VIKEN J K, et al. Design and performance of the NASA SCEPTOR distributed electric propulsion flight demonstrator[C]∥ 16th AIAA Aviation Technology, Integration, and Operations Conference. Reston: AIAA, 2016. |
39 | STOLL A M, BEVIRT J, MOORE M D, et al. Drag reduction through distributed electric propulsion[C]∥ 14th AIAA Aviation Technology, Integration, and Operations Conference. Reston: AIAA, 2014. |
40 | VELDHUIS L M. Propeller wing aerodynamic interference[D]. Delft: Delft University of Technology, 2005. |
41 | 杨伟, 范召林, 吴文华, 等. 考虑滑流影响的分布式螺旋桨布局优化设计[J]. 空气动力学学报, 2021, 39(3): 71-79. |
YANG W, FAN Z L, WU W H, et al. Optimal design of distributed propeller layout considering slipstream effect[J]. Acta Aerodynamica Sinica, 2021, 39(3): 71-79 (in Chinese). | |
42 | 王科雷, 周洲, 祝小平, 等. 低雷诺数多螺旋桨/机翼耦合气动设计[J]. 航空学报, 2018, 39(8): 121918. |
WANG K L, ZHOU Z, ZHU X P, et al. Multi-propeller/wing coupled aerodynamic design at low Reynolds number[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(8): 121918 (in Chinese). | |
43 | WANG H B, GAN W B, LI D C. An investigation of the aerodynamic performance for a propeller-aided lift-enhancing double wing configuration[J]. Aerospace Science and Technology, 2020, 105: 105991. |
44 | 王红波. 基于动力诱导增升垂直起降气动设计研究[D]. 西安: 西北工业大学, 2018: 63-97. |
WANG H B. Aerodynamic design of vertical takeoff and landing based on dynamic induced lift[D].Xi'an: Northwestern Polytechnical University, 2018: 63-97 (in Chinese) . | |
45 | 石清. 机翼增升减阻的流动控制研究[D]. 长沙: 国防科技大学, 2017: 63-100. |
SHI Q. Study on flow control of wing lift and drag reduction[D].Changsha: National University of Defense Technology, 2017: 63-100 (in Chinese) . | |
46 | JIRÁSEK A. Vortex-generator model and its application to flow control[J]. Journal of Aircraft, 2004, 42: 1486-1491. |
47 | BRUNET V, FRANÇOIS C, GARNIER E, et al. Experimental and numerical investigations of vortex generators effects: AIAA-2006-3027 [R]. Reston:AIAA, 2006. |
48 | GODARD G, STANISLAS M. Control of a decelerating boundary layer. Part 1: Optimization of passive vortex generators[J]. Aerospace Science and Technology, 2006, 10(3): 181-191. |
49 | 张惠, 赵宗德, 周广鑫, 等. 涡发生器参数对风力机翼型性能影响实验研究[J]. 太阳能学报, 2017, 38(12): 3399-3405. |
ZHANG H, ZHAO Z D, ZHOU G X, et al. Experimental investigation of effect of vortex generator’s parameter on performance of wind turbine aerofoil[J]. Acta Energiae Solaris Sinica, 2017, 38(12): 3399-3405 (in Chinese). | |
50 | 宗昕. 大型飞机机翼增升减阻技术研究[D]. 南京: 南京航空航天大学, 2012: 41-59. |
ZONG X. Research on wing lift and drag reduction technology of large aircraft[D].Nanjing: Nanjing University of Aeronautics and Astronautics, 2012: 41-59 (in Chinese). | |
51 | VELDHUIS L, VERVOORT E. Drag effect of a dented surface in a turbulent flow[C]∥ Proceedings of the 27th AIAA Applied Aerodynamics Conference. Reston: AIAA, 2009. |
52 | BEVES C C, BARBER T J. Aerofoil flow separation suppression using dimples[J]. The Aeronautical Journal, 2011, 115(1168): 335-344. |
53 | 焦雪文, 张立茹, 牛佳佳, 等. 低雷诺数下凹坑结构对翼型层流分离影响的数值研究[J]. 可再生能源, 2021, 39(3): 346-352. |
JIAO X W, ZHANG L R, NIU J J, et al. Numerical study on the influence of dimples structure on airfoil laminar flow separation under low Reynolds number[J]. Renewable Energy Resources, 2021, 39(3): 346-352 (in Chinese). | |
54 | WAHIDI R, BRIDGES D H. Effects of distributed suction on an airfoil at low Reynolds number[J]. AIAA Journal, 2012, 50(3): 523-539. |
55 | 刘沛清, 马利川, 屈秋林, 等. 低雷诺数下翼型层流分离泡及吹吸气控制数值研究[J]. 空气动力学学报, 2013, 31(4): 518-524, 540. |
LIU P Q, MA L C, QU Q L, et al. Numerical investigation of the laminar separation bubble control by blowing/suction on an airfoil at low Re number[J]. Acta Aerodynamica Sinica, 2013, 31(4): 518-524, 540 (in Chinese). | |
56 | 邓雄, 赵志杰, 王秋旺, 等. 基于前缘合成双射流的飞翼布局纵向气动控制特性研究[J]. 空气动力学学报, 2022, 40(5): 79-90. |
DENG X, ZHAO Z J, WANG Q W, et al. Research on longitudinal aerodynamic control characteristics of flying wing based on leading-edge dual synthetic jets[J]. Acta Aerodynamica Sinica, 2022, 40(5): 79-90 (in Chinese). | |
57 | LIAN Y S, SHYY W, VIIERU D, et al. Membrane wing aerodynamics for micro air vehicles[J]. Progress in Aerospace Sciences, 2003, 39(6-7): 425-465. |
58 | 李冠雄, 马东立, 杨穆清, 等. 低雷诺数翼型局部振动非定常气动特性[J]. 航空学报, 2018, 39(1): 121427. |
LI G X, MA D L, YANG M Q, et al. Unsteady aerodynamic characteristics of airfoil with local oscillation at low Reynolds number[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 121427 (in Chinese). | |
59 | 娄斌. 低空太阳能无人机设计及增升减阻技术研究[D]. 杭州: 浙江大学, 2019: 72-94. |
LOU B. Design of low-altitude solar unmanned aerial vehicle and research on lift and drag reduction technology[D].Hangzhou: Zhejiang University, 2019: 72-94 (in Chinese). | |
60 | ZHA G C, PAXTON C. A novel airfoil circulation augment flow control method using co-flow jet[C]∥ 2nd AIAA Flow Control Conference. Reston: AIAA, 2004. |
61 | 张顺磊, 杨旭东, 宋笔锋, 等. 应用协同射流原理的旋翼翼型增升减阻试验研究[J]. 航空工程进展, 2021, 12(4): 44-51, 67. |
ZHANG S L, YANG X D, SONG B F, et al. Experimental investigation of lift enhancement and drag reduction of rotor airfoil using co-flow jet concept[J]. Advances in Aeronautical Science and Engineering, 2021, 12(4): 44-51, 67 (in Chinese). | |
62 | 宋超, 杨旭东, 朱敏, 等. 应用离散型协同射流的翼型增升减阻研究[J]. 西北工业大学学报, 2015, 33(2): 191-196. |
SONG C, YANG X D, ZHU M, et al. Investigating lift increase and drag reduction for airfoils using discrete CFJ(co-flow jet)[J]. Journal of Northwestern Polytechnical University, 2015, 33(2): 191-196 (in Chinese). | |
63 | 于金革, 牛中国, 梁华, 等. 等离子体用于飞翼布局模型增升减阻试验研究[J]. 空气动力学学报, 2015, 33(6): 823-827. |
YU J G, NIU Z G, LIANG H, et al. Experimental investigation on flying wing lift enhancement and drag reduction by plasma[J]. Acta Aerodynamica Sinica, 2015, 33(6): 823-827 (in Chinese). | |
64 | 阳鹏宇, 张鑫, 赖庆仁, 等. 机翼尺度效应对等离子体分离流动控制特性的影响[J]. 力学学报, 2021, 53(12): 3321-3330. |
YANG P Y, ZHANG X, LAI Q R, et al. Experimental investigation of the influence of scaling effects of wings on the flow separation control using plasma actuators[J]. Chinese Journal of Theoretical and Applied Mechanics, 2021, 53(12): 3321-3330 (in Chinese). | |
65 | LARRABEE E. Practical design of minimum induced loss propellers[R]. 1979. |
66 | D’ANGELO S, BERARDI F, MINISCI E. Aerodynamic performances of propellers with parametric considerations on the optimal design[J]. The Aeronautical Journal, 2002, 106(1060): 313-320. |
67 | MORGADO J, ABDOLLAHZADEH M, SILVESTRE M A R, et al. High altitude propeller design and analysis[J]. Aerospace Science and Technology, 2015, 45: 398-407. |
68 | 项松, 王吉, 张利国, 等. 一种高效率螺旋桨设计方法[J]. 航空动力学报, 2015, 30(1): 136-141. |
XIANG S, WANG J, ZHANG L G, et al. A design method for high efficiency propeller[J]. Journal of Aerospace Power, 2015, 30(1): 136-141 (in Chinese). | |
69 | 梁撑刚, 郁新华, 龚军锋. 一种无人机螺旋桨的快速优化设计方法[J]. 航空计算技术, 2017, 47(2): 76-79. |
LIANG C G, YU X H, GONG J F. A quick approach to optimum design of UAV propeller[J]. Aeronautical Computing Technique, 2017, 47(2): 76-79 (in Chinese). | |
70 | 刘芳,杜绵银,岳良明. 高空低雷诺数高效螺旋桨设计[C]∥ 第三届中国航空科学技术大会,2017:15-21. |
LIU F, DU M Y, YUE L M. High efficiency propeller design at low Reynolds number and high altitude[C]∥The 3rd China Aeronautical Science and Technology Conference, 2017:15-21 (in Chinese). | |
71 | 刘坤澎,王海峰,江泓鑫,等. 螺旋桨多设计点气动优化方法和变桨距角策略[J]. 航空学报, 2023,40:doi:10.7527/S1000-6893.2023.28831. |
LIU K P, WANG H F, JIANG H X, et al. Aerodynamic optimization method of propeller multi-design points and variable pitch angle strategy[J]. Acta Aeronautica et Astronautica Sinica, 2023, 40:doi:10.7527/S1000-6893.2023.28831. | |
72 | WEI Y L, QIAN Y J, BIAN S Y, et al. Experimental study of the performance of a propeller with trailing-edge serrations[J]. Acoustics Australia, 2021, 49(2): 305-316. |
73 | 朱敏, 杨旭东, 宋超, 等. 应用协同射流控制的临近空间螺旋桨高增效方法[J]. 航空学报, 2014, 35(6): 1549-1559. |
ZHU M, YANG X D, SONG C, et al. High synergy method for near space propeller using co-flow jet control[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6): 1549-1559 (in Chinese). | |
74 | 李玉杰, 罗振兵, 邓雄, 等. 合成双射流控制NACA0015翼型大攻角流动分离试验研究[J]. 航空学报, 2016, 37(3): 817-825. |
LI Y J, LUO Z B, DENG X, et al. Experimental investigation on flow separation control of stalled NACA0015 airfoil using dual synthetic jet actuator[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3): 817-825 (in Chinese). | |
75 | 程钰锋, 李洪亮, 祝方正. 临近空间介质阻挡放电特性及其提高螺旋桨性能的数值分析[J]. 飞机设计, 2016, 36(5): 7-14. |
CHENG Y F, LI H L, ZHU F Z. Numerical study on the characteristics of the dielectric barrier discharge and plasma to enhance propeller characteristics in near space[J]. Aircraft Design, 2016, 36(5): 7-14 (in Chinese). |
[1] | Haifeng WANG, Kunpeng LIU, Hongxin JIANG, Chenxi DU. Aerodynamic optimization method of propeller multi⁃design points and variable pitch angle strategy [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 528831-528831. |
[2] | Xiaofei YANG, Tailu SUN, Dejun MENG, Haibao YIN, Yongmei WANG. Aerodynamic design method for core⁃driven fan stage considering multiple modes [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(2): 128625-128625. |
[3] | Xianzhong GAO, Xiaolong DENG, Yujie WANG, Zheng GUO, Zhongxi HOU. General planning method for energy optimal flight path of solar⁃powered aircraft in near space [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 27265-027265. |
[4] | Xiaolong DENG, Xixiang YANG, Bingjie ZHU, Zhenyu MA, Zhongxi HOU. Simulation research and key technologies analysis of intelligent stratospheric aerostat Loon [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127412-127412. |
[5] | Chunpeng LI, Zhansen QIAN, Xiasheng SUN. Trailing edge deformation matrix aerodynamic design for long-range civil aircraft variable camber wing [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 127335-127335. |
[6] | Junhong LI, Xuhong JIN, Chunfeng LIU, Wenbo MIAO, Xiaoli CHENG. Microaerodynamic experiment and computation of near space high speed vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127072-127072. |
[7] | Yuhong CUI, Yizhe XU, Fanxi LYU, Fei ZHAO, Yujia ZHANG, Jiameng SUN, Guang ZUO. Influencing factors of weapon separation of hypersonic vehicles in near space [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(24): 128539-128539. |
[8] | Xuhui ZHANG, Chunlei XIE, Sijia LIU, Ming YAN, Siyuan XING. Development needs and difficulty analysis for smart morphing aircraft [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 529302-529302. |
[9] | Xiaofeng WANG, Feng QU, Junjie FU, Zeyu WANG, Chaoyu LIU, Junqiang BAI. Discrete adjoint-based aerodynamic design optimization for hypersonic inward turning inlet [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 128352-128352. |
[10] | Zhiguang SHI, Yujie YANG, Zongyu ZUO. Multi-element coupled modeling and simulation for multi-capsule near-space airships [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(16): 228451-228451. |
[11] | Jiameng SUN, Guang ZUO, Yizhe XU, Ruofan DU, Yuhong CUI. Numerical simulation of weapon delivery schemes for hypersonic vehicles in near space [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(13): 127808-127808. |
[12] | Haoge LI, Hua YANG, Yuxin YANG, Weifang CHEN. Refinement optimization design for heat reduction on windward surface of hypersonic lifting body [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 124-137. |
[13] | LIN Peng, ZHUANG Fujian, QU Linfeng, XU Yangyang, SU Yadong. Technological development in hypersonic nozzle design, manufacture and validation: A review [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 526160-526160. |
[14] | BO Juntian, WANG Guohong, YU Hongbo, ZHANG Xiangyu. Track-before-detection algorithm for multiple hypersonic targets in near space [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 325299-325299. |
[15] | BO Juntian, WANG Guohong, YU Hongbo, ZHANG Xiangyu. Algorithm for detecting and positioning hypersonic targets with wakes in near space [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(5): 325255-325255. |
Viewed | ||||||
Full text |
|
|||||
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341