CFD Calculation of a Helicopter Rotor Hovering in Ground Effect (English)
- New search for: Kutz, Benjamin M.
- New search for: Bensing, Felix
- New search for: Keßler, Manuel
- New search for: Krämer, Ewald
- New search for: Dillmann, Andreas
- New search for: Heller, Gerd
- New search for: Kreplin, Hans-Peter
- New search for: Nitsche, Wolfgang
- New search for: Peltzer, Inken
- New search for: Kutz, Benjamin M.
- New search for: Bensing, Felix
- New search for: Keßler, Manuel
- New search for: Krämer, Ewald
In:
New Results in Numerical and Experimental Fluid Mechanics VIII
: Contributions to the 17th STAB/DGLR Symposium Berlin, Germany 2010
;
Chapter: 36
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297-304
;
2013
- Article/Chapter (Book) / Electronic Resource
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Title:CFD Calculation of a Helicopter Rotor Hovering in Ground Effect
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Additional title:Notes Numerical Fluid Mech.
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Contributors:Dillmann, Andreas ( editor ) / Heller, Gerd ( editor ) / Kreplin, Hans-Peter ( editor ) / Nitsche, Wolfgang ( editor ) / Peltzer, Inken ( editor ) / Kutz, Benjamin M. ( author ) / Bensing, Felix ( author ) / Keßler, Manuel ( author ) / Krämer, Ewald ( author )
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Published in:New Results in Numerical and Experimental Fluid Mechanics VIII : Contributions to the 17th STAB/DGLR Symposium Berlin, Germany 2010 ; Chapter: 36 ; 297-304Notes on Numerical Fluid Mechanics and Multidisciplinary Design ; 121 ; 297-304
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Publisher:
- New search for: Springer Berlin Heidelberg
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Place of publication:Berlin, Heidelberg
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Publication date:2013-01-01
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Size:8 pages
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ISBN:
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ISSN:
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DOI:
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Type of media:Article/Chapter (Book)
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Type of material:Electronic Resource
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Language:English
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Keywords:
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Source:
Table of contents eBook
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Investigation of the Impact of Simplifying the Aircraft Geometry on the Characteristics of the Vertical TailplaneKröhnert, Anna / Gebhardt, Lutz et al. | 2013
- 2
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Aerodynamic Optimization of a High-Lift System with Kinematic ConstraintsFranke, Dirk M. et al. | 2013
- 3
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Simulation of Store Separation Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical SimulationsSchade, N. et al. | 2013
- 4
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Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet ConfigurationRonzheimer, Arno / Hepperle, Martin / Brezillon, Joël / Brodersen, Olaf / Lieser, Jan et al. | 2013
- 5
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Analytical Design of an Inlet Distortion Generator and Its Experimental and Numerical ValidationLesser, Andreas / Schulze, Sonja / Niehuis, Reinhard / Kähler, Christian / Lieser, Jan et al. | 2013
- 6
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Wake Measurements to Assess the Flow-Structure Interaction of an Elasto-flexible Morphing Wing ConfigurationBeguin, B. / Breitsamter, C. / Adams, N. et al. | 2013
- 7
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Aerodynamic Characteristics of the Blended Wing Body ACFA2020Meyer, Michael / Breitsamter, Christian et al. | 2013
- 8
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Development of the Adjoint Approach for Aeroelastic Wing OptimizationAbu-Zurayk, Mohammad / Brezillon, Joël et al. | 2013
- 9
-
Application of a Coupling of Flight Mechanics and Aerodynamics to Predict the SHEFEX I Ascent PhaseBartolomé Calvo, J. / Wolkow, S. / Eggers, Th. et al. | 2013
- 10
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Experimental and Numerical Analysis of SHEFEX-IIBarth, Tarik / Gehre, Rolf / Eggers, Thino / Schramm, Jan Martinez / Wagner, Alexander / Hannemann, Klaus / Kaufmann, Rene / Böhrk, Hannah et al. | 2013
- 11
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Investigation on Turbulence Structures in the Wake of a Generic Rocket ConfigurationWolf, C. Christian / Henke, Rolf / Hörnschemeyer, Ralf et al. | 2013
- 12
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Thermal Fluid-Structure-Interaction on a Flat-Plate Model in Hypersonic High-Enthalpy FlowCostantini, M. / Esser, B. / Gülhan, A. et al. | 2013
- 13
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Numerical Generation of a Flush Air Data System for the Hypersonic Flight Experiment HIFiRE 7Bode, C. / Eggers, Th. / Smart, M. et al. | 2013
- 14
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Characterization of a Free-Molecular Pressure Probe Employing Gas-Kinetic SimulationGrabe, Martin / Dettleff, Georg / Boettcher, Rolf-D. / Hannemann, Klaus et al. | 2013
- 15
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Wind Tunnel and Flight Tests with Active Flow Control on a S10 Glider ConfigurationGrund, T. / Nitsche, W. et al. | 2013
- 16
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Evaluation of Passive and Active Secondary Flow Control in a High Speed Compressor Cascade with Different Measurement TechniquesLiesner, Karsten / Meyer, Robert et al. | 2013
- 17
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Parameter Study for a Slatless 2D High-Lift Airfoil with Active Separation Control Using a URANS ApproachCiobaca, V. et al. | 2013
- 18
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Influence of the Actuator Jet Angle on the Reattachment Process with Pulsed ExcitationHecklau, M. / Salazar, D. Pieren / Nitsche, W. et al. | 2013
- 19
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Optimal Control of a Plane Jet Using the Adjoint MethodMarinc, Daniel / Foysi, Holger et al. | 2013
- 20
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Investigation of Active Flow Control Using a Differential Reynolds Stress ModelTogiti, V. / Ciobaca, V. / Eisfeld, B. et al. | 2013
- 21
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Experimental and Numerical Modeling of Flow around Perforated Stabilizing DevicesChernukha, P. A. / Raffel, M. / Kalugin, V. T. et al. | 2013
- 22
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Investigations on Active Drag Control on a Bluff Body with Cross-WindKrentel, Daniel / Nitsche, Wolfgang et al. | 2013
- 23
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Investigation of the Wear Properties of a Riblet Paint Structure on an Airbus A300-600ST BelugaHage, Wolfram / Stenzel, Volkmar / Vynnyk, Taras et al. | 2013
- 24
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Experimental Investigation of Oscillating Riblets for Turbulent Drag ReductionGrüneberger, René / Kramer, F. / Hage, Wolfram / Meyer, R. / Thiele, F. / Wassen, E. et al. | 2013
- 25
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Preliminary Numerical Assessment of Turbulent Flow Control with Plasma ActuatorsCriscione, A. / Frohnapfel, B. / Tropea, C. et al. | 2013
- 26
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Performance Reduction of Dielectric Barrier Discharge Plasma Actuators at Higher Mach NumbersKriegseis, Jochen / Grundmann, Sven / Tropea, Cameron et al. | 2013
- 27
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Investigation of Transitional Flow Structures Downstream of a Backward-Facing-Step by Using 2D-2C- and High Resolution 3D-3C- Tomo- PIVSchröder, A. / Schanz, D. / Heine, B. / Dierksheide, U. et al. | 2013
- 28
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Direct Numerical Simulation of Tollmien-Schlichting Waves to Support Linear Stability AnalysisLüdeke, Heinrich / Wartemann, Viola / Seitz, Arne et al. | 2013
- 29
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Direct Numerical Simulation of Crossflow-Transition Control Using Pinpoint SuctionFriederich, Tillmann A. / Kloker, Markus J. et al. | 2013
- 30
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Introduction of Initial Seeds for Subharmonic Resonance by Modulation of T-S Waves in an Airfoil Boundary LayerDe Paula, I. B. / Würz, W. / Krämer, E. / Borodulin, V. I. / Kachanov, Y. S. et al. | 2013
- 31
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Active Tollmien Schlichting Wave Control with a Membrane Actuator in Compressible FlowsErdmann, Ralf / Leuckert, Janin / Rosemann, Henning / Nitsche, Wolfgang et al. | 2013
- 32
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Active Transition Delay by Spatial Surface Actuation with Model Predictive ControlPätzold, A. / Peltzer, I. / Nitsche, W. / Goldin, N. / King, R. / Haller, D. / Woias, P. et al. | 2013
- 33
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Probability of Occurrence of the Turbulent Flow Structures in Transitional Pipe FlowsKrauss, J. / Ertunç, Ö. / Ostwald, Ch. / Lienhart, H. / Delgado, A. et al. | 2013
- 34
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Development of a Numerical Simulation Platform to Improve the Prediction of Helicopter Blade Vortex Interaction (BVI)Schneider, S. et al. | 2013
- 35
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Numerical Investigation of Pulsed Air Jets for Dynamic Stall Control on the OA209 AirfoilGardner, A. D. / Knopp, T. / Richter, K. / Rosemann, H. et al. | 2013
- 36
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CFD Calculation of a Helicopter Rotor Hovering in Ground EffectKutz, Benjamin M. / Bensing, Felix / Keßler, Manuel / Krämer, Ewald et al. | 2013
- 37
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Numerical Simulation of a Complete Helicopter Configuration in Forward Flight Using Fluid-Structure CouplingKhier, Walid et al. | 2013
- 38
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RANS-Based Laminar-Turbulent Transition Prediction for Airfoil and Rotary Wing Applications Using Semi-empirical CriteriaHeister, C. C. / Klein, A. / Krämer, E. et al. | 2013
- 39
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Visualization and Computation of Quantified Density Data of the Rotor Blade Tip VortexHernandez, R. / Heine, B. / Schneider, O. / Chernukha, P. / Raffel, M. et al. | 2013
- 40
-
CFD Based Methods for the Computation of Generalized Aerodynamic ForcesFleischer, Dietmar / Breitsamter, Christian et al. | 2013
- 41
-
Nonlinear Numerical Flight Dynamics of Flexible Aircraft in the Time Domain by Coupling of CFD, Flight Mechanics, and Structural MechanicsRitter, Markus et al. | 2013
- 42
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Numerical Experiments on Aerodynamic Resonance in Transonic Airfoil FlowNitzsche, Jens / Giepman, Rogier H. M. et al. | 2013
- 43
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Extension of an Aeroelastic Coupling Environment to Aircraft Configurations with Rigid-Body Degrees of FreedomWellmer, Georg / Behr, Marek / Ballmann, Josef et al. | 2013
- 44
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Coupled CFD-CSM Simulations of Aerostabil Windtunnel Experiments, Considering Structural Shell ModellingStickan, Bernd / Dillinger, Johannes / Schewe, Günter et al. | 2013
- 45
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Lax-Wendroff and Cell-Vertex Upwind DiscretizationsRossow, C. -C. et al. | 2013
- 46
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Accuracy in a Finite Volume Godunov Type MethodBauer, Maria / Birken, Philipp / Hannemann, Volker / Oßwald, Kai et al. | 2013
- 47
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Conservative, Skew–Symmetric Discretization of the Compressible Navier–Stokes EquationsReiss, Julius / Sesterhenn, Jörn et al. | 2013
- 48
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Grid–Induced Uncertainties in Wake Regions and a Local Refinement Method for Hexahedral LayersMazlum, Ekrem / Probst, Axel / Radespiel, Rolf et al. | 2013
- 49
-
Continuous Formulation of Wall Function with Adverse Pressure GradientRöber, Thomas et al. | 2013
- 50
-
Point and Line Implicit Methods to Improve the Efficiency and Robustness of the DLR TAU CodeLanger, Stefan et al. | 2013
- 51
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Accuracy of the Cell-Centered Grid Metric in the DLR TAU-CodeSchwöppe, Axel / Diskin, Boris et al. | 2013
- 52
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Vortical Modeling in the DLR TAU CodeWeinman, K. A. et al. | 2013
- 53
-
A Discrete Adjoint Approach for Unsteady Optimal Flow ControlNemili, Anil / Özkaya, Emre / Gauger, Nicolas R. / Carnarius, Angelo / Thiele, Frank et al. | 2013
- 54
-
An Algebraic Sensor for the RANS-LES Switch in Delayed Detached-Eddy SimulationKnopp, Tobias / Probst, Axel et al. | 2013
- 55
-
A Zonal RANS/LES Method for the Flow Around an Airfoil at High Angle of AttackGeurts, K. J. / Meinke, M. / Schröder, W. et al. | 2013
- 56
-
Fluid-Structure-Interaction Applying a Ghost-Cell Immersed Boundary MethodHylla, Eike / Thiele, Frank et al. | 2013
- 57
-
A Level-Set Based Cartesian Grid Method to Simulate In-Cylinder FlowGünther, Claudia / Hartmann, Daniel / Meinke, Matthias / Schröder, Wolfgang et al. | 2013
- 58
-
Aerodynamic Inverse Design Framework Using Discrete Adjoint MethodBrezillon, Joël / Abu-Zurayk, Mohammad et al. | 2013
- 59
-
Higher-Order and Adaptive Discontinuous Galerkin Methods Applied to Turbulent Delta Wing FlowHartmann, Ralf et al. | 2013
- 60
-
Development of a Parallel Fluid-Structure Coupling Environment and Application to a Wind Tunnel Model under High Aerodynamic LoadsSpiering, Frank / Heinrich, Ralf / Keye, Stefan et al. | 2013
- 61
-
Influence of Wing Elasticity on the Experimental and Numerical Determination of Dynamic DerivativesHübner, A. -R. / Kilian, T. / Spiering, F. et al. | 2013
- 62
-
Numerical Simulation of Wind Tunnel Wall Effects on the Transonic Flow around an Airfoil ModelRichter, K. / Rosemann, H. et al. | 2013
- 63
-
Aspects of the Industrialization of Automatic Transition Prediction for Three-Dimensional Configurations with the eN-MethodKrimmelbein, Normann / Krumbein, Andreas / Togiti, Vamshi et al. | 2013
- 64
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Comparison of a Local Correlation-Based Transition Model with an eN-Method for Transition PredictionSeyfert, Cornelia / Krumbein, Andreas et al. | 2013
- 65
-
Simulations of a Compressor Cascade with Steady Secondary Flow SuctionLemke, M. / Gmelin, C. / Thiele, F. et al. | 2013
- 66
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Influence of a Hub-Groove on the Unsteady Losses of a Transonic Compressor StageRochhausen, Stefan / Kröger, Georg / Nicke, Eberhard / Stollenwerk, Stefan et al. | 2013
- 67
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Numerical Simulation of Engine-Inlet Stall with Advanced Physical Modelling Compared to Validation ExperimentsProbst, Axel / Schulze, Sonja / Radespiel, Rolf / Kähler, Christian J. et al. | 2013
- 68
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Numerical Investigation of Hot and Cold Side Jet Interaction with a Supersonic Cross-FlowHöld, Roland K. / Engert, Marcus / Weinand, Klaus / Stern, Dirk et al. | 2013
- 69
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Lattice-Boltzmann Solutions with Local Grid Refinement for Nasal Cavity FlowsLintermann, A. / Eitel-Amor, G. / Meinke, M. / Schröder, W. et al. | 2013
- 70
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Numerical Simulation of the Oscillatory Ventilation in Simplified Human Lung ModelsFeldmann, Daniel / Wagner, Claus et al. | 2013
- 71
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Direct Numerical Simulation of Non-Oberbeck-Boussinesq Effects in Turbulent Rayleigh-Bénard Convection of WaterHorn, Susanne / Shishkina, Olga / Wagner, Claus et al. | 2013
- 72
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Turbulent Convection in a Rayleigh-Bénard Cell with Solid Horizontal Plates of Finite ConductivityCzarnota, T. / Wagner, C. et al. | 2013
- 73
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Computations of Mixed and Displacement Ventilation in an Aircraft CabinWebel, O. / Rütten, M. / Wagner, C. et al. | 2013
- 74
-
Particle Reconstruction with Optical Transfer Functions Applied to Tomo-PIV-ExperimentsSchanz, D. / Gesemann, S. / Schröder, A. / Wienecke, B. et al. | 2013
- 75
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Comparison of PIV Measured Flow Structures in Two Four-Valve Piston EnginesBücker, I. / Karhoff, D. / Dannemann, J. / Pielhop, K. / Klaas, M. / Schröder, W. et al. | 2013
- 76
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Transition Measurement with Microstructured Hot Film Sensor Arrays on a Laminar Flow Airfoil ModelRiedl, X. / Leuckert, J. / Engert, M. / Kupke, W. / Wagner, R. / Nitsche, W. / Abbas, A. / Bauer, K. et al. | 2013
- 77
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Comparative Imaging Pressure and Wall Shear Stress Measurements on a Circular CylinderRudolph, Ilka / Dobriloff, Christoph / Domhardt, Jan / Nitsche, Wolfgang et al. | 2013
- 78
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Investigation of Circular Cylinder Flow in Water Using Temperature-Sensitive PaintFey, U. / Klein, C. / Möller, T. J. / Pöttner, J. / Radespiel, R. / Ondrus, V. / Beifuß, U. et al. | 2013
- 79
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Investigation of Aero-Optical Effects in Model Deformation Measurements in a Transonic FlowKirmse, Tania / Gardner, Anthony / Krombholz, Christian et al. | 2013
- 80
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A Method for Optical Measurements of Height Distributions in Transparent MediaLenk, Sebastian / Westhoff, Andreas / Wagner, Claus et al. | 2013
- 81
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Experimental Investigation of Flow Structure Formation in a Heated Duct FlowMey, Tobias / Westhoff, Andreas / Wagner, Claus et al. | 2013
- 82
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Cavity Simulations Using an Explicit Discontinuous Galerkin Scheme with Local Time-SteppingTaube, Arne / Gassner, Gregor / Munz, Claus-Dieter et al. | 2013
- 83
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Advances in Numerical Aeroacoustics with the Discontinuous Galerkin Solver NoisSolBirkefeld, Andreas / Munz, Claus-Dieter et al. | 2013
- 84
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Optimal Control to Reduce Supersonic Jet NoiseSchulze, J. / Sesterhenn, J. et al. | 2013
- 85
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Pylon Trailing Edge Blowing for the Control of CROR Unsteady Blade LoadsStuermer, Arne / Yin, Jianping et al. | 2013
- 86
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Particle Image Velocimetry of the Underbody Flow of Generic High-Speed TrainsJönsson, Mattias / Loose, Sigfried / Wagner, Claus et al. | 2013
- 87
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Scaling of the Aeroacoustics of High-Speed TrainsLauterbach, Andreas / Loose, Sigfried / Ehrenfried, Klaus et al. | 2013
- 88
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Numerical Simulation of Train-Tunnel Entry Using a BEM in Time DomainWagner, Sebastian / Ehrenfried, Klaus / Dillmann, Andreas et al. | 2013