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    Multi-Objective Aerodynamic and Aeroelastic Coupled Design Optimization Using a Full Viscosity Discrete Adjoint Harmonic Balance Method 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 010:;page 101002-1
    Author(s): Wu, Hangkong; Wang, Dingxi; Huang, Xiuquan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: With increasing requirements for high-loading and high-efficiency turbomachines, blades become thinner and thinner and thus design optimizations considering both aerodynamic performances and aeroelastic stability become ...
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    Three-Dimensional Unsteady Aerodynamic Optimization of a Transonic Compressor Stage Using an Implicit Discrete Adjoint Harmonic Balance Method 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 007:;page 71016-1
    Author(s): Wu, Hangkong; Wang, Dingxi; Huang, Xiuquan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The design of high-loading and compact modern turbomachines results in strong unsteady interactions between two adjacent blade rows, which has been found to have a noticeable impact on aerodynamic performances of turbomachines. ...
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    A Time–Space Multigrid Method for Efficient Solution of the Harmonic Balance Equation System 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 009:;page 091006-1
    Author(s): Wu, Hangkong; Wang, Dingxi; Huang, Xiuquan; Xu, Shenren
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this article, an efficient time–space multigrid (TS-MG) method for solving the harmonic balance (HB) equation system is proposed. The principle of the time–space multigrid method is to coarsen grids in both space and ...
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