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    Application of Adjoint-Enhanced First Order Second Moment Method for Robust Design Optimization of a High Pressure Compressor Rotor 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 002:;page 21010-1
    Author(s): Dittmann, Max; Schmidt, Robin; Meyer, Marcus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper applies the computationally advantageous combination of a differential analysis technique and the adjoint method in the context of uncertainty quantification to the gradient-based robust design optimization of ...
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    Prediction of Steady and Unsteady Flow Quantities Using Multiscale Graph Neural Networks 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 007:;page 71015-1
    Author(s): Strönisch, Sebastian; Sander, Maximilian; Meyer, Marcus; Knüpfer, Andreas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Analysis, optimization, and uncertainty quantification of the aerodynamic behavior of turbomachinery components is a fundamental part of the current industrial design process and requires the extensive use of compute-intensive ...
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    Employing the Time-Domain Unsteady Discrete Adjoint Method for Shape Optimization of Three-Dimensional Multirow Turbomachinery Configurations 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 008:;page 81006
    Author(s): Ntanakas, Georgios; Meyer, Marcus; Giannakoglou, Kyriakos C.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In turbomachinery, the steady adjoint method has been successfully used for the computation of derivatives of various objective functions with respect to design variables in gradient-based optimization. However, the ...
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    Roughness Investigations on In-Service High-Pressure Compressor Blades—Part I: An Automated Process for High-Fidelity Roughness Measurements 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008:;page 81001-1
    Author(s): Vasilopoulos, Ilias; Rostamian, Mirco; Voigt, Matthias; Meyer, Marcus; Mailach, Ronald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The two-part publication deals with roughness investigations on in-service high-pressure compressor (HPC) blades, both in terms of measurements and simulations. In this article (Part I), an automated process for performing ...
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    Comparison of Two Methods for Sensitivity Analysis of Compressor Blades 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 011:;page 111006
    Author(s): Schmidt, Robin; Voigt, Matthias; Vogeler, Konrad; Meyer, Marcus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper will compare two approaches of sensitivity analysis, namely (i) the adjoint method which is used to obtain an initial estimate of the geometric sensitivity of the gas-washed surfaces to aerodynamic quantities ...
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    Probabilistic Finite Element Analysis of Cooled High-Pressure Turbine Blades—Part A: Holistic Description of Manufacturing Variability 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 010:;page 0101008-1
    Author(s): Högner, Lars; Voigt, Matthias; Mailach, Ronald; Meyer, Marcus; Gerstberger, Ulf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Modern high-pressure turbine (HPT) blade design stands out due to its high complexity comprising three-dimensional blade features, multipassage cooling system (MPCS), and film cooling to allow for progressive thermodynamic ...
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    A Methodology for a Coupled Structural–Computational Fluid Dynamics Analysis of Compressor Rotor Blades Subjected to Ice Impact With Uncertain Impactor Parameters 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 003:;page 31001-1
    Author(s): Böhm, Holger; Högner, Lars; Meyer, Marcus; Mailach, Ronald; Hornig, Andreas; Gude, Maik
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method for a coupled structural–computational fluid dynamics (CFD) analysis of a compressor rotor blade subjected to an ice impact scenario is investigated to assess the impact related blade deformations from a structural ...
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    Probabilistic Finite Element Analysis of Cooled High-Pressure Turbine Blades—Part B: Probabilistic Analysis 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 010:;page 0101009-1
    Author(s): Högner, Lars; Voigt, Matthias; Mailach, Ronald; Meyer, Marcus; Gerstberger, Ulf
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Modern high-pressure turbine (HPT) blade design stands out due to high complexity comprising three-dimensional blade features, multipassage cooling system (MPCS), and film cooling to allow for progressive thermodynamic ...
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    Robust Design Optimization of a Compressor Rotor Using Recursive Cokriging Based Multi-Fidelity Uncertainty Quantification and Multi-Fidelity Optimization 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 006:;page 61009-1
    Author(s): Wiegand, Marcus; Prots, Andriy; Meyer, Marcus; Schmidt, Robin; Voigt, Matthias; Mailach, Ronald
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work focuses on the application of multi-fidelity methods for the robust design optimization of engine components. The robust design optimization approach yields geometric designs that have high efficiencies and are ...
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    Convergence Acceleration of Favre-Averaged Non-Linear Harmonic Method 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 002:;page 21002-1
    Author(s): Wang, Feng; Weber, Kurt; Radford, David; di Mare, Luca; Meyer, Marcus
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper develops a numerical procedure to accelerate the convergence of the Favre-averaged non-linear harmonic (FNLH) method. The scheme provides a unified mathematical framework for solving the sparse linear systems ...
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