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    Chapter and Conference Paper

    Dynamic Load Balancing of a Coupled Lagrange Particle Tracking Solver for Direct Injection Engine Application

    A dynamic load balancing technique for multiphysics simulation methods based on hierarchical Cartesian meshes for a direct injection internal combustion engine application is presented. A finite-volume method ...

    Tim Wegmann, Matthias Meinke, Wolfgang Schröder in Sustained Simulation Performance 2022 (2024)

  2. No Access

    Chapter and Conference Paper

    Analysis of the hot gas ingress into the wheel space of an axial turbine stage

    The thermal efficiency of gas turbines strongly depends on the turbine inlet temperature. Increasing the inlet gas temperature improves the engine performance, but results in new challenges for the cooling of ...

    Jannik Borgelt, Thomas Hösgen in High Performance Computing in Science and … (2023)

  3. No Access

    Chapter

    On the Use of Active Pre-chambers and Bio-hybrid Fuels in Internal Combustion Engines

    Pre-chamber combustion systems combined with bio-hybrid fuels allow for an efficiency increase of internal combustion engines and a reduction of engine-out emissions. Experimental and numerical investigations ...

    Patrick Burkardt, Maximilian Fleischmann in Engines and Fuels for Future Transport (2022)

  4. No Access

    Chapter and Conference Paper

    Comparison of Two Airfoils for Active Drag Reduction in Turbulent Flow

    Active flow control of the turbulent flow over two airfoils of different shape is performed with the goal of increasing the overall aerodynamic efficiency. Large-eddy simulations are performed to investigate t...

    Marian Albers, Matthias Meinke in High Performance Computing in Science and … (2021)

  5. No Access

    Chapter and Conference Paper

    Drag Reduction by Surface Actuation

    The flow over an DRA2303 wing section is controlled by spanwise traveling transversal surface waves. The actuated flow field is investigated by large-eddy simulation. Approximately

    Marian Albers, Matthias Meinke in High Performance Computing in Science and … (2021)

  6. No Access

    Chapter and Conference Paper

    Numerical Investigation of a Porous Trailing Edge by a Zonal RANS/LES Simulation

    A hybrid Reynolds-averaged Navier-Stokes (RANS)/large-eddy simulation (LES) approach for flows with porous surfaces is presented. For the two-dimensional geometry considered, a computationally cheap 2D-RANS si...

    Sutharsan Satcunanathan, Matthias Meinke in New Results in Numerical and Experimental … (2021)

  7. No Access

    Chapter and Conference Paper

    Numerical Analysis of Ethanol and 2-Butanone Direct Injection in an Internal Combustion Engine

    The mixture formation of air and the gasoline surrogates Ethanol and 2-Butanone is numerically investigated using large-eddy simulations of the direct-injection into an internal combustion engine. The multiphy...

    Tim Wegmann, Sven Berger, Matthias Meinke in High Performance Computing in Science and … (2021)

  8. Chapter

    Numerical Analysis of the Turbulent Wake for a Generic Space Launcher with a Dual-Bell Nozzle

    The turbulent wake of an axisymmetric generic space launcher equipped with a dual-bell nozzle is simulated at transonic ( \(Ma_\infty = 0.8\) and \(Re_D = 4.3\cdot 10^5\) ) and supersonic ( \(Ma_\infty = 3\) a...

    Simon Loosen, Matthias Meinke in Future Space-Transport-System Components u… (2021)

  9. No Access

    Chapter and Conference Paper

    Dynamic Load Balancing for Coupled Simulation Methods

    A dynamic load balancing technique for simulation methods based on hierarchical Cartesian meshes is presented for two applications in this paper. The first method is a hybrid CFD/CAA solver for the prediction ...

    Matthias Meinke, Ansgar Niemöller in Sustained Simulation Performance 2019 and … (2021)

  10. No Access

    Chapter and Conference Paper

    The Direct-Hybrid Method for Computational Aeroacoustics on HPC Systems

    Classic hybrid methods for computational aeroacoustics use different solvers and methods to predict the flow field and the acoustic pressure field in two separate steps, which involves data exchange via disk I...

    Michael Schlottke-Lakemper, Hans Yu, Sven Berger in High-Performance Scientific Computing (2017)

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    Chapter and Conference Paper

    Validation of Particle-Laden Large-Eddy Simulation Using HPC Systems

    In this contribution, results of a direct particle-fluid simulation (DPFS) are compared with direct numerical simulations and large-eddy simulations (LES) using a popular Euler-Lagrange method (ELM). DPFS faci...

    Konstantin Fröhlich, Lennart Schneiders in Sustained Simulation Performance 2017 (2017)

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    Chapter and Conference Paper

    Interaction of Acoustic and Entropy Waves with Shocks

    of and entropy waves with an oblique shock occurring upstream of a cone is investigated. The three-dimensional supersonic Ma \(=\) = 5.9 flow over a \(30^{\circ }\) 30 ∘ half angle cone...

    Thomas Schilden, Matthias Meinke in New Results in Numerical and Experimental … (2016)

  13. No Access

    Chapter and Conference Paper

    Towards Adjoint-Based Trailing-Edge Noise Minimization Using Porous Material

    In this paper, we present a discrete adjoint-based optimization framework to obtain the optimal distribution of the porous material over the trailing edge of a 3-D flat plate. The near-body strength of the noi...

    Beckett Y. Zhou, Nicolas R. Gauger in New Results in Numerical and Experimental … (2016)

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    Chapter and Conference Paper

    Large-Eddy Simulation of the Flow Field in a Rotating Axial Fan

    Large-eddy simulation (LES) results of the turbulent flow field in a \(72^{\circ }\) ...

    Alexej Pogorelov, Matthias Meinke in New Results in Numerical and Experimental … (2016)

  15. No Access

    Chapter and Conference Paper

    Aeroacoustic Simulations of Ducted Axial Fan and Helicopter Engine Nozzle Flows

    The flow and the acoustic field of an axial fan and a helicopter engine jet are computed by a hybrid fluid dynamics – computational aeroacoustics method. For the predictions of the flow field a high-fidelity, ...

    Alexej Pogorelov, Mehmet Onur Cetin in High Performance Computing in Science and … (2016)

  16. No Access

    Chapter and Conference Paper

    Investigation of the Effect of a Realistic Nozzle Geometry on the Jet Development

    Highly resolved large-eddy simulations (LES) of a helicopter engine jet including the nozzle geometry are performed. A flow solver for compressible flow based on hierarchically refined Cartesian meshes and a c...

    Mehmet Onur Cetin, Matthias Meinke in Proceedings of the 5th International Confe… (2016)

  17. No Access

    Chapter and Conference Paper

    Simulation of a Helicopter Engine Jet Including a Realistic Nozzle Geometry

    of a helicopter engine jet at a Reynolds number of Re = 750,000 and a Mach number of M = 0.341 is performed. The influence of a realistic nozzle geometry on the jet properties is analyzed by using hig...

    Mehmet Onur Cetin, Matthias Meinke in New Results in Numerical and Experimental … (2016)

  18. No Access

    Chapter and Conference Paper

    Large-Scale Simulations of a Non-generic Helicopter Engine Nozzle and a Ducted Axial Fan

    Large-eddy simulations (LESs) of a helicopter engine jet and an axial fan are performed by using locally refined Cartesian hierarchical meshes. For the computations a high-fidelity, massively parallelized solv...

    Mehmet Onur Cetin, Alexej Pogorelov in High Performance Computing in Science and … (2016)

  19. No Access

    Chapter and Conference Paper

    A Hybrid Discontinuous Galerkin-Finite Volume Method for Computational Aeroacoustics

    A hybrid method for a fully coupled determination of aerodynamic sound is introduced. From the instantaneous velocity and vorticity, determined by approximate solutions of the Navier-Stokes equations, acoustic...

    Michael Schlottke-Lakemper, Matthias Meinke in New Results in Numerical and Experimental … (2016)

  20. No Access

    Chapter and Conference Paper

    CFD/CAA Simulations on HPC Systems

    In this paper, a highly scalable numerical method is presented that allows to compute the aerodynamic sound from a turbulent flow field on HPC systems. A hybrid CFD-CAA method is used to compute the flow and t...

    Michael Schlottke-Lakemper, Fabian Klemp in Sustained Simulation Performance 2016 (2016)

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