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    Experimental Investigation on the Effects of Inlet Circumferential Distortion and Optimized Casing Treatment in a Transonic Compressor 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:007
    Author(s): Fan, Zhonggang; Xu, Xiaobin; Zhang, Min; Ba, Dun; Liu, Yang; Du, Juan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Casing treatment has been widely adopted to enhance the operating range of compressors by extending the stall margin. In this article, a high-precision experimental investigation is conducted in a transonic ...
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    Generative Inverse Aerodynamic Design of a Single-Stage Turbine Using Conditional Denoising Diffusion Probabilistic Model 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:004:;page 814
    Author(s): Wu, Yueteng; Zhang, Min; Xu, Xiaobin; Yin, Yue; Ba, Dun; Du, Juan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. The aerodynamic design of turbomachinery is crucial for the overall performance of aero engines and has long been a paramount field of research. Traditional design methods are categorized into forward and inverse ...
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    Experimental Investigations on the Effects of Surface Roughness for Compressor Cascades With Different Roughness Magnitude and Location 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003:;page 31007-1
    Author(s): Yu, Xianjun; Zhao, Shouyang; An, Guangfeng; Xu, Yuhang; Xu, Xiaobin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Blade surface roughness could significantly affect the aerodynamic performance of compressors. To explore the influence of roughness magnitude and location on blade performance, experiments were conducted in a low-speed ...
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