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    Computer 3D Vision-Aided Full-3D Optimization of a Centrifugal Impeller 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 009:;page 91011-1
    Author(s): Ji, Cheng; Wang, Zhiheng; Xi, Guang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A computer three-dimensional (3D) vision-aided performance prediction framework for turbomachinery is established in this paper, to improve the accuracy and generalization ability of the artificial neural network (ANN) ...
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    Experimental Investigation on the Aerodynamic Instability Process of a High-Speed Axial-Centrifugal Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 008:;page 81018-1
    Author(s): Li, Jiaan; Wang, Baotong; Zheng, Xuedong; Wang, Zhiheng; Zheng, Xinqian
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aerodynamic instability plays an important role in compressor design and may cause performance degradation and fatigue damage. In this paper, an experimental study on the evolution of aerodynamic instability is carried out ...
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    Adaptive Batch Sampling Strategy for the Hundreds-Dimensional Aerodynamic Optimization of the Centrifugal Impeller 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 009:;page 91003-1
    Author(s): Ji, Cheng; Wang, Zhiheng; Xi, Guang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In recent years, in order to achieve higher performance, the number of design variables used in the aerodynamic optimization of turbomachinery (based on surrogate models) has increased significantly. However, the increase ...
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    A Flow Information-Based Prediction Model Applied to the Nonaxisymmetric Hub Optimization of a Centrifugal Impeller 

    Source: Journal of Mechanical Design:;2021:;volume( 143 ):;issue: 010:;page 0103502-1
    Author(s): Ji, Cheng; Wang, Zhiheng; Tang, Yonghong; Xi, Guang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A full-range prediction model for turbomachinery based on the flow-field information code is established in this article to solve the problems that traditional models do not have enough prediction accuracy and cannot reflect ...
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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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