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    Application of the Improved Incremental Nonlinear Dynamic Inversion in Fixed-Wing UAV Flight Tests 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 006:;page 04022091
    Author(s): Zhenchang Liu; Yufei Zhang; JianJian Liang; Haixin Chen
    Publisher: ASCE
    Abstract: Incremental nonlinear dynamic inversion shows good robustness and low dependence on the model information. In this study, incremental nonlinear dynamic inversion is improved and utilized to solve the six-degrees-of-freedom ...
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    Aerodynamic Optimization and Noise Reduction of a Two-Stage Series Compact Fan 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 005:;page 04021057-1
    Author(s): Shaoguang Zhang; Runze Li; Yufei Zhang; Haixin Chen
    Publisher: ASCE
    Abstract: This paper focused on the aerodynamic optimization and noise reduction of a two-stage series compact fan. The space constraints of compact fans limit the design space, which poses several challenges to aerodynamic and noise ...
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    Numerical Investigation of Premature Stall in a Non-Tip-Loaded Rotor Caused by Circumferential Groove Casing Treatment 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 004:;page 04021032-1
    Author(s): Yutian Liang; Weimin Song; Haixin Chen; Yufei Zhang
    Publisher: ASCE
    Abstract: Casing treatment design and application typically focus on improving stall margin while minimizing efficiency penalty for tip-loaded rotors. When successful casing treatment configurations are found, it often is assumed ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian