Showing 1 - 20 results of 107 for search 'Research and Analysis Wing', query time: 0.08s Refine Results
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    Design and Coupling Dynamics Research of a Single-drive Multi-mode Flapping-wing Aircraft by Jiang Houqing, Hou Yu, Guo Yongxing

    Published 2023-11-01
    “…Through the kinematic and aerodynamic coupling analysis of the combined mechanism, the coupling dynamic characteristics of the flapping-wing aircraft are obtained, which provides a research basis for the flight control and performance improvement of the flapping-wing aircraft in the future.…”
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    Structural Design and Experiment Analysis of a Morphing Wing Structure by Song Zhendong, Li Gang, Guo Bing

    Published 2020-03-01
    “…The optimization algorithm is used to optimize the morphing wing structure. On the basis of theoretical research, the experimental prototype is processed and the related experimental tests are carried out.…”
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    Analysis of clogging factors in single-wing labyrinth drip irrigation tape. by Hui Zhang, Hongfei Tao, Yao Liu, Qiao Li, Youwei Jiang, Mahemujiang Aihemaiti, Wenxin Yang

    Published 2024-01-01
    “…In this paper, we designed a uniform orthogonal test to study the effects of fertilizer concentration, sediment content and working pressure on the clogging of single-wing labyrinth drip irrigation tapes. The observed data from the experiment were analysed and calculated using range analysis, variance analysis, and main-effect multiple comparison analysis, then the optimal working conditions were determined. …”
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    Control Characteristics Analysis of Multi-Section Morphing Wing Based on Centroid Self-Trimming by Hang Ma, Zhongbin Zhou, Dingshan Zhang

    Published 2025-01-01
    “…Based on the research on the sweep angle change of the elbow and hand wing sections during the flight of large birds, this paper proposes a multi-section variable-sweep wing structure suitable for large-scale UAVs. …”
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    Geometrical Nonlinear Aeroelastic Stability Analysis of a Composite High-Aspect-Ratio Wing by Chang Chuan Xie, Jia Zhen Leng, Chao Yang

    Published 2008-01-01
    “…Planar doublet lattice method is used to calculate unsteady aerodynamics in frequency domain ignoring the bending effect of the deflected wing. And then, the aeroelastic stability analysis of the system under a given load condition is successively carried out. …”
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    Fatigue Experiment and Failure Mechanism Analysis of Aircraft Titanium Alloy Wing–Body Connection Joint by Xianmin Chen, Shanshan Li, Yuanbo Liang, Shuo Wang, Liang Yan, Shichang Du

    Published 2024-12-01
    “…Taking the titanium alloy wing–body connection joint at the rear beam of a certain type of aircraft as the research object, this study analyzed the failure mechanism and verified the structural safety of the wing–body connection joint under actual flight loads. …”
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    UNFOLDING PERFORMANCE OF FOLDING WING FOR ACTUATOR AND EXPERIMENT by LIU DuanChen, HAN XueFeng, ZHANG Yue, ZHANG MingYue, LIU XiaoDong

    Published 2017-01-01
    “…In order to study the parameters of a folding wing‘s spreading performance which is used on the guided missile’s actuator,the unfolding performance was researched. …”
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    DYNAMICS ANALYSIS AND LIGHTWEIGHT DESIGN OF BIONIC ROBOTIC FISH FRAME MECHANISM (MT) by LI XingShan, QIAO Jie, LI MingHao

    Published 2023-01-01
    “…The caudal fin mechanism was introduced into ADAMS environment for dynamic analysis, and the motion load of the bionic robotic fish frame mechanism was obtained. …”
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    Article
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    Development of Anisogrid Lattice Composite Structures for Fighter Wing Applications by Muhammad Kusni, Bambang Kismono Hadi, Leonardo Gunawan, Hendri Syamsudin

    Published 2024-01-01
    “…This paper presents research on the use of anisogrid lattice structures in fighter wing applications. …”
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    Conceptual Design of an Unmanned Fixed-Wing Aerial Vehicle Based on Alternative Energy by Alan G. Escobar-Ruiz, Omar Lopez-Botello, Luis Reyes-Osorio, Patricia Zambrano-Robledo, Luis Amezquita-Brooks, Octavio Garcia-Salazar

    Published 2019-01-01
    “…In fact, the aerodynamic analysis is obtained for a preliminary design; this step involves the wing, fuselage, and empennage of the UAV. …”
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    Computational assessment of winglet-induced variations in pressure coefficients on NACA 4418 aircraft wings by Md. Abdullah, Mohammad Zoynal Abedin

    Published 2025-01-01
    “…This study presents a computational analysis of the effects of winglets on the aerodynamic performance of NACA 4418 aircraft wings, focusing on the variations in pressure coefficients. …”
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    Design and fabrication study of a small remote-controlled bionic butterfly flapping-wing flying machine by Yaozeng Mao, Fan Wu, Junjie Lao, Minglei Li

    Published 2024-12-01
    “… This research is devoted to simulating the flight characteristics of real butterflies, and a small remote-controlled bionic butterfly flying machine is designed and manufactured. …”
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