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    Effect of Rubber Strain Rate on Performance of Aircraft Tire 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 002:;page 04022002
    Author(s): Yu Gan; Xiaohui Wei; Xingbo Fang
    Publisher: ASCE
    Abstract: An aircraft tire is a kind of rubber product with a complex structure. When subjected to impact load, the mechanical properties of rubber material on strain history and strain rate cannot be ignored. According to the ...
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    Aerodynamic Design Optimization of a Staggered Rotors Octocopter Based on Surrogate Model 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 004:;page 04021036-1
    Author(s): He Zhu; Hong Nie; Limao Zhang; Siqiang Deng; Xiaohui Wei
    Publisher: ASCE
    Abstract: Improving aerodynamic performance with limited dimensions is becoming more important in the design of multirotor aircraft. Complex coupling interactions exist between the structural parameters and aerodynamic performance ...
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    Nonlinear Assembly Tolerance Design for Spatial Mechanisms Based on Reliability Methods 

    Source: Journal of Mechanical Design:;2017:;volume( 139 ):;issue: 003:;page 32301
    Author(s): Yin, Yin; Hong, Nie; Fei, Feng; Xiaohui, Wei; Huajin, Ni
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Assembly tolerance design for spatial mechanisms is a complex engineering problem that involves a highly nonlinear dimension chain equation and challenges in simplifying the spatial mechanism matrix equation. To address ...
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    Crashworthiness Performance Simulation and Analysis of Combined-Type Landing Gear Buffer 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 004:;page 04022049
    Author(s): Xingbo Fang; Hu Chen; Yuying Han; Xinhong Xie; Xiaohui Wei; Hong Nie
    Publisher: ASCE
    Abstract: To improve the crashworthiness of the landing gear buffer, an oleo-pneumatic buffer combined with an expansion tube is proposed in this paper. A numerical analytical model based on deformation theory was used to acquire ...
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    Bifurcation Characteristics of Emergency Extension of a Landing Gear Mechanism Considering Aerodynamic Effect 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 005:;page 04021046-1
    Author(s): Yin Yin; Yixin Yang; Kui Xu; Hong Nie; Xiaohui Wei
    Publisher: ASCE
    Abstract: The emergency extension system for nose landing gear (NLG) is vitally important for safe landing in the event of hydraulic source failure. To study the dynamic properties of NLG emergency extension, it is necessary to ...
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    DSpace software copyright © 2002-2015  DuraSpace
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