| Citation: | Yu Junli, Wang Linlin, Gao Geet al. Investigation of aerodynamic characteristics on saucer-shaped lifting-body[J]. Journal of Beijing University of Aeronautics and Astronautics, 2010, 36(2): 198-201. (in Chinese)
|
|
[1] Katz J,Byrne S,Hahl R.Stall resistance features of lifting body airplane configurations .AIAA-98-16581,1998 [2] Wood R M,Bauer S X S.Flying wings/flying fuselages .AIAA-2001-0311,2001 [3] Mitchell K A.Burnelli and his Lifting-body transports[J].American Aviation Historical Society Journal,1997,4:2-19 [4] Hiroshi Kawato,Shigeya Watanabe,Yukimitsu Yamamoto,et al.Aerodynamic design of a lifting-body type reentry vehicle .AIAA-2003-7059,2003 [5] 吴希拴,师小娟,王建培.无人机翼尖小翼参数优化及风洞试验研究[J].飞行力学,2004,22(1): 30-36 Wu Xishuan,Shi Xiaojuan.Data optimization and wind tunnel test of UAV winglets[J].Flight Dynamics,2004,22(1):30-36(in Chinese) [6] 邓彦敏,胡继忠.轻型飞机翼梢减阻外形的风洞实验研究[J].航空学报,1994,15(8): 897-903 Deng Yanmin,Hu Jizhong.Experimental research of the configuration of wing-tip drag reducing for light aircraft[J].Acta Aeronoutica et Astronautica Sinica,1994,15(8): 897-903(in Chinese) [7] 李建华,李锋.低雷诺数反齐默曼机翼的气动特性[J].计算物理,2007,24(1): 49-53 Li Jianhua,Li Feng.Simulation of an inverse zimmerman wing at low reynolds numbers[J].Chinese Journal of Computational Physics,2007,24(1): 49-53 (in Chinese) [8] 上官云信,周瑞兴,高永卫,等.翼型相对厚度对失速分离特性的影响[J].空气动力学学报,2000,18:21-26 Shangguan Yunxin,Zhou Ruixing,Gao Yongwei,et al.The effect of relative thickness of airfoil on stall separate character[J].Acta Aerodynamica Sinica,2000,18:21-26 (in Chinese)
|
| [1] | CHENG Y，ZHAO J R，HUANG S L，et al. Research on dynamic characteristics of distributed multi-rotor/tilting wing aeroelastic coupling[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（5）：1637-1650 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0253. |
| [2] | WANG Wei, CUI Shenao, CHEN Jiahua, ZHAO Haoxiang, ZHANG Zhen. Research status and progress of bionic groove drag reduction[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0898 |
| [3] | WANG Y T，LIU Y，WANG H，et al. Drag reduction characteristics analysis of variable camber based on plane parameters of blended wing body configuration[J]. Journal of Beijing University of Aeronautics and Astronautics，2025，51（2）：525-545 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2023.0011. |
| [4] | SU Jinxin, XI Ziyan, DAI Yuting. Nonlinear fluid-structure interaction response analysis of a large flexible wing under strong gusts[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0278 |
| [5] | LI Keyu, YANG Chao, WANG Xiaozhe, WAN Zhiqiang, LI Chang. Aeroelastic optimization of wing structure and material using multiple microstructures[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0178 |
| [6] | YE Yi-qiao, SHEN Hai-dong, LIU Yan-bin, GAO Ze-peng, KONG Xiang, CHEN Jin-bao. Integrated design of hypersonic aircraft wing layout and mission trajectory[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0650 |
| [7] | LIU Y H，HUANG Y，TAN H，et al. On-line prediction method of wing flexible baseline based on autoregressive model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（11）：3426-3433 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0865. |
| [8] | ZHANG Y M，DAI Y T，WEI R K，et al. Experiment on dynamic response alleviation of a wing with variable-camber flexible trailing edge[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（10）：3239-3249 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0761. |
| [9] | WANG Ziang, LU Zhirong, LI Honghao, ZHOU Wenya, WANG Xiaoming. SMA driven multi-state variable camber wing: Design，analysis，and experimentation[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0844 |
| [10] | MAO Junjie, QU Guoxin, GAO Zhenxun. Numerical investigation of heat and drag reduction by discrete microholes film in hypersonic flow[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0443 |
| [11] | XIAO L F，ZHOU L W，LI X D. Numerical simulation of deformed airfoil modal after blast shock wave[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（1）：341-349 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2022.0244. |
| [12] | LEI Chao-hui, YANG Chao, SONG Chen. Optimization design of active aeroelastic wing with variable camber[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0623 |
| [13] | ZHOU Quan-zhi, YANG You-xu, SUN Lu-bin, ZHANG Xing-cui, WU Yi-fei, HUO Meng-wen. Aeroelastic Optimization Design of SpaRibs Wing Structure[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0343 |
| [14] | XIE C C，ZHU L P，MENG Y，et al. Design of adaptive deformation wing control system based on system identification[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2761-2770 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0717. |
| [15] | XING Xiao-bing, TAN Jian-feng, YANG Yu-xiao, YONG Tian, YU Ling-jun, WU Rui. An efficient analysis method of helicopter fuselage bullet damage based on bullet penetration theory[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2023.0450 |
| [16] | YANG K L，HAN D. Influence of rotor/wing aerodynamic interference on performance of compound helicopters[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（7）：1761-1771 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0561. |
| [17] | WANG L，ZENG T H，REN Z F，et al. Analysis of heat load and bleed air schedule for hot air anti-icing system[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（10）：2660-2668 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0710. |
| [18] | LYU Z Y，NIE X Y，ZHAO A B. Prediction of wing aerodynamic coefficient based on CNN[J]. Journal of Beijing University of Aeronautics and Astronautics，2023，49（3）：674-680 （in Chinese）. doi: 10.13700/j.bh.1001-5965.2021.0276. |
| [19] | HONG Zheng, YE Zhengyin. Numerical investigation on evolution of T-S wave on a two-dimensional compliant wall with finite length[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(7): 1190-1199. doi: 10.13700/j.bh.1001-5965.2021.0030 |
| [20] | LIU Mingjie, WU Qingshan, YAN Hao, YU Cunming, LIN Cunguo, ZHANG Jinwei, ZHAO Tianyi. Progress and challenges of bionic drag reduction surfaces[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(9): 1782-1790. doi: 10.13700/j.bh.1001-5965.2022.0295 |
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
LANG Bo, HUANG Rui, LI Wei-qinet al. Methods of Integrating and Constructing Distributed Service Objects on Web[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(2): 149-152. (in Chinese)
DownLoad: