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    Anomalous Data Detection for Roller-Integrated Compaction Measurement 

    Source: International Journal of Geomechanics:;2016:;Volume ( 016 ):;issue: 001
    Author(s): Zhi-hong Nie; Xiang Wang; Tan Jiao
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents a theoretical and experimental analysis of an anomalous data detection treatment for roller-integrated compaction measurement (RICM) data. Anomalous data, which may be discovered during the collection ...
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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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    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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    Impact Analysis of Lunar Lander Soft Landing Performance Caused by the Body Gravity Centerline Shift 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    Author(s): Qing Lin; Zhiyu Kang; Jie Ren; Qilong Zhao; Hong Nie
    Publisher: American Society of Civil Engineers
    Abstract: In order to obtain the lunar lander soft landing performance impact caused by the body gravity centerline shift, a seven-degree-of-freedom dynamic model is established based on the inertia force, and a dynamics and kinematics ...
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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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    Damping Force Analysis and Optimization of a Lunar Lander with MRF 

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 003
    Author(s): Chen Wang; Hong Nie; Jinbao Chen; Heow Pueh Lee
    Publisher: ASCE
    Abstract: Controllable lunar landers with magnetorheological fluid (MRF) damper have become a hot topic of research. However, limited research studies have been performed on the damping force analysis of MRF under high-velocity ...
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    DSpace software copyright © 2002-2015  DuraSpace
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