1–16 von 16 Ergebnissen
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    Aerodynamic optimisation of a winglet-cavity tip in a high-pressure axial turbine cascade

    Zhou, Zhihua / Chen, Shaowen / Wang, Songtao | SAGE Publications | 2018

    A comparison of different unsteady flow control techniques in a highly loaded compressor cascade

    Zhang, Hongxin / Chen, Shaowen / Gong, Yun et al. | SAGE Publications | 2019

    Numerical investigation of boundary layer suction on certain highly loaded aspirated compressor at low speeds

    Chen, Shaowen / Zhou, Zhihua / Wang, Songtao et al. | SAGE Publications | 2018

    The compound bowing design in a highly loaded linear cascade with large turning angle

    Xue, Xingxu / Wang, Songtao / Luo, Lei et al. | SAGE Publications | 2020

    Design method of rail grinding target profile based on non-uniform rational B-spline

    Lin, Fengtao / Wang, Songtao / Zhang, Hai et al. | SAGE Publications | 2021

    The effect of different clearance geometry configurations on aerodynamic performance in a high-load compressor cascade

    Chen, Shaowen / Sun, Shijun / Lan, Yunhe et al. | SAGE Publications | 2014

    Design method of worn rail grinding profile based on Frechet distance method

    Lin, Fengtao / Zou, Liang / Yang, Yang et al. | SAGE Publications | 2022

    Effects of a sweeping jet actuator on aerodynamic performance in a linear turbine cascade with tip clearance

    Chen, Shaowen / Li, Weihang / Meng, Qinghe et al. | SAGE Publications | 2019

    Experimental study on axially non-uniform clearances in a linear turbine cascade with a cavity squealer tip

    Chen, Shaowen / Meng, Qinghe / Li, Weihang et al. | SAGE Publications | 2019

    Cooling structure design of gas turbine blade by using multi-level highly efficient design platform

    Zhao, Zhiqi / Luo, Lei / Li, Shouzuo et al. | SAGE Publications | 2021

    Experiment study of the winglet-cavity tip on the aerodynamic performance in a turbine cascade

    Chen, Shaowen | Online Contents | 2017
    Beteiligte: Wang, Songtao