1–19 von 19 Ergebnissen
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    Effects of inlet radial distortion on the type of stall precursor in low-speed axial compressor

    Arshad, Ali / Li, Qiushi / Li, Simin et al. | SAGE Publications | 2018

    Flapping wing device and aircraft

    Freier Zugriff
    ZHENG MENGZONG / PAN TIANYU / LIANG JINZE et al. | Europäisches Patentamt | 2023

    Energy management method and energy adjustment method for gas-electric hybrid power system

    Freier Zugriff
    PAN TIANYU / LI ZHIPING / ZHAO YANG et al. | Europäisches Patentamt | 2021

    Helicopter rotor dynamic stall control structure based on imitated whale fin leading edge

    Freier Zugriff
    LI ZHIPING / PAN TIANYU / HOU YUFEI et al. | Europäisches Patentamt | 2020

    Parallel differential two-degree-of-freedom flapping wing mechanism

    Freier Zugriff
    PAN TIANYU / ZHENG MENGZONG / PENG LIANSONG et al. | Europäisches Patentamt | 2020

    Tilting rotor wing with bionic wavy front edge and tilting rotorcraft

    Freier Zugriff
    LI ZHIPING / PAN TIANYU / HE LONG et al. | Europäisches Patentamt | 2021

    Study on the aerodynamic performance of boundary-layer-ingesting inlet with various geometries

    Li, Zhiping / Zhang, Yafei / Pan, Tianyu et al. | SAGE Publications | 2022

    Bionic flapping wing device and aircraft

    Freier Zugriff
    PAN TIANYU / LIANG JINZE / ZHENG MENGZONG et al. | Europäisches Patentamt | 2023

    Power supply control system applied to vehicle-mounted power supply device

    Freier Zugriff
    SONG DEZHOU / PAN TIANYU / SHU XIAOMING et al. | Europäisches Patentamt | 2021

    Flapping wing structure and aircraft

    Freier Zugriff
    SU GUANTING / PAN TIANYU / LIANG JINZE et al. | Europäisches Patentamt | 2024

    Catastrophe-Theory-Based Modeling of Airfoil-Stall Boundary at Low Reynolds Numbers

    Li, Zhiping / Zhang, Peng / Pan, Tianyu et al. | AIAA | 2017