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    Detecting Multidimensional Pareto Fronts During the Optimization of a Return Channel Within a Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2021:;volume( 144 ):;issue: 004:;page 41003-1
    Author(s): Bisping, Jan; Jeschke, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: We explain the advantages of using big-data methods for evaluating numerical optimization. The investigation focuses on the performance potential of three-dimensional return channel vanes under realistic manufacturing ...
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    A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 007:;page 71010
    Author(s): Jeschke, Peter; Penkner, Andreas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A gas generator—consisting of a singlestage shrouded mixedflow compressor without a diffusor, a rotating combustion chamber, and a vaneless singlestage shrouded centripetal turbine—is presented and analyzed here. All ...
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    Advanced Rayleigh Pressure Loss Model for High Swirl Combustion in a Rotating Combustion Chamber 

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 002:;page 21502
    Author(s): Penkner, Andreas; Jeschke, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the effect of excessive total pressure losses for heat transfer problems in fluid flows with a high circumferential swirl component. At RWTH Aachen University, a novel gas generator concept is under ...
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    Rotor-Alone Tones in the Outflow Noise of a Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 011:;page 0111001-1
    Author(s): Faßbender, Armin; Enneking, Martin; Jeschke, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article investigates the generation of rotor-alone tones and their contribution to the outflow noise of a transonic centrifugal compressor stage with vaneless diffuser and volute by means of unsteady full-annulus ...
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    Teaching Aero-Engine Performance: From Analytics to Hands-On Exercises Using Gas Turbine Performance Software 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 001:;page 11015-1
    Author(s): Jeschke, Peter; Koschel, Wolfgang; Klumpp, Christian; Weintraub, Daniel
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we present an approach for teaching turbojet engine performance that combines mathematical analysis with the use of performance software to provide students with a comprehensive and in-depth understanding ...
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    Experimental Investigation of a Truncated Pipe Diffuser With a Tandem Deswirler in a Centrifugal Compressor Stage 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 003:;page 31019
    Author(s): Kunte, Robert; Jeschke, Peter; Smythe, Caitlin
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The subject of this paper is the experimental investigation of three different geometric configurations of the diffusing system in a high pressure centrifugal compressor stage for a jet engine application. The objective ...
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    Numerical Investigation of the Unsteady Flow Inside a Centrifugal Compressor Stage With Pipe Diffuser 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 003:;page 31012
    Author(s): Grates, Daniel R.; Jeschke, Peter; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The subject of this paper is the investigation of unsteady flow inside a transonic centrifugal compressor stage with a pipediffuser by utilizing unsteady 3D Reynoldsaveraged Navier–Stokes simulations (unsteady 3D URANS). ...
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    Evaluation of Measurement Uncertainties for Pneumatic Multihole Probes Using a Monte Carlo Method 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 007:;page 72605
    Author(s): Hölle, Magnus; Bartsch, Christian; Jeschke, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The subject of this paper is a statistical method for the evaluation of the uncertainties for pneumatic multihole probe measurements. The method can be applied to different types of evaluation algorithms and is suitable ...
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    Influence of Purge Flow Injection on the Performance of an Axial Turbine With Three-Dimensional Airfoils and Non-Axisymmetric Endwall Contouring 

    Source: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 006:;page 61004-1
    Author(s): Schäflein, Lukas; Janssen, Johannes; Brandies, Henri; Jeschke, Peter; Behre, Stephan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we present the evaluation of the aerodynamic robustness to rim seal purge flow of an optimized 1.5-stage axial turbine configuration with a bowed stator profile and endwall contouring. Performance maps ...
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    Accuracy of Steady Pneumatic Probes in Unsteady Turbomachinery Flows 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 011:;page 111014-1
    Author(s): Widera, Tim Sebastian; Patzer, Bastian; Behre, Stephan; Jeschke, Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study shows that no additional measurement error due to unsteadiness was detected, when measuring in periodic turbomachinery flows at frequencies up to 5 kHz with steady, pneumatic probes. An experiment was designed, ...
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