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    Mechanisms of Banner Cloud Formation 

    Source: Journal of the Atmospheric Sciences:;2013:;Volume( 070 ):;issue: 011:;page 3631
    Author(s): Voigt, Matthias; Wirth, Volkmar
    Publisher: American Meteorological Society
    Abstract: anner clouds are clouds in the lee of steep mountains or sharp ridges. Their formation has previously been hypothesized as due to three different mechanisms: (i) vertical uplift in a lee vortex (which has a horizontal ...
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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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    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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    Roughness Investigations on In-Service High-Pressure Compressor Blades—Part II: Roughness Parameterization and Computational Fluid Dynamics-Based Modeling of Its Impact on Turbulent Flows 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008:;page 81002-1
    Author(s): Vasilopoulos, Ilias; Adami, Paolo; 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 paper (Part II), first, stripe measurements of surface ...
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    Comprehensive Geometric Description of Manufacturing Scatter of High-Pressure Turbine Nozzle Guide Vanes for Probabilistic CFD Analysis 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 08:;page 81002
    Author(s): Voigt, Paul; Högner, Lars; Fiedler, Barbara; Voigt, Matthias; Mailach, Ronald; Meyer, Marcus; Nasuf, Alkin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The increasing demands on jet engines require progressive thermodynamic process parameters, which typically lead to higher aerothermal loadings and accordingly to designs with high complexity. State-of-the-art high-pressure ...
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    Comprehensive Geometric Description of Manufacturing Scatter of High-Pressure Turbine Nozzle Guide Vanes for Probabilistic CFD Analysis 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 008:;page 81002
    Author(s): Voigt, Paul; Högner, Lars; Fiedler, Barbara; Voigt, Matthias; Mailach, Ronald; Meyer, Marcus; Nasuf, Alkin
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: The increasing demands on jet engines require progressive thermodynamic process parameters, which typically lead to higher aerothermal loadings and accordingly to designs with high complexity. State-of-the-art high-pressure ...
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