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    Chapter and Conference Paper

    Interaction of Wing-Tip Vortices and Jets in the Extended Wake

    The interaction of wing-tip vortices and jets in the extended wake is experimentally and numerically investigated. The measurements focus on the unsteady wake of a swept-wing half-model equipped with an engine...

    Frank T. Zurheide, Guido Huppertz in Summary of Flow Modulation and Fluid-Struc… (2010)

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    Chapter

    A Level-Set Based Cartesian Grid Method to Simulate In-Cylinder Flow

    This work discusses the extension of a three-dimensional, strictly conservative Cartesian cut-cell based method to meet the requirements for the simulation of in-cylinder flow and other flows bounded by comple...

    Claudia Günther, Daniel Hartmann in New Results in Numerical and Experimental … (2013)

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    Chapter

    Numerical Investigation of the Combined Effects of Gravity and Turbulence on the Motion of Small and Heavy Particles

    Numerical studies [1, 2] show that the influence of gravity and turbulence on the motion of small and heavy particles is not a simple superposition. However, in [3] it is shown that these studies may be artifi...

    Christoph Siewert, Rudie Kunnen in New Results in Numerical and Experimental … (2014)

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    Chapter

    Partitioned Fluid-Structure Interaction on Solution-Adaptive Hierarchical Cartesian Grids

    A solution-adaptive hierarchical Cartesian cut-cell method is validated for fluid-structure interaction problems involving rigid bodies. The response of a tandem configuration of elastically supported cylin...

    Gonzalo Brito Gadeschi, Matthias Meinke in New Results in Numerical and Experimental … (2014)

  5. No Access

    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)

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    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)

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    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)

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    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)

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    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)

  11. 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)