New results in numerical and experimental fluid mechanics III : contributions to the 12th STAB/DGLR symposium, Stuttgart, Germany, 2000 / Siegfried Wagner [and others] (editors).

Includes bibliographical references.

Design Work for the A3XX High-Lift-Wing -- Recent Improvements in the Measurement of Aerodynamic Damping Derivatives -- Calculation of Horizontal Stabilizer Efficiency with a Navier-Stokes Code -- 3D RANS Simulations for High-Lift Analysis of Transport Aircraft Configurations -- Numerical Investigation of the Reynolds-Number-Effect on the Setting Sensitivity of a 2D High-Lift Multi-Element Airfoil -- Separation Control on a High-Lift Configuration by Periodic Exitation -- Numerical Investigation of the Effect of the High-Lift Configuration of a Transport Aircraft on its Vortex Wake -- The Relationship Between Near- and Far-Field of Vortex Wakes from Aircraft with High Aspect Ratio Wings -- Influence of Different Flap Settings on the Hazard Posed to Following Aircraft -- Numerical Simulation of Wake-Vortex Encounters Using the Chimera-Technique -- Aspects of Low Speed Wind Tunnel Testing on an A400M Model with Propeller Simulation -- Coupling of DLR Navier-Stokes Solver FLOWer with an e[superscript N]-Database Method for Laminar-Turbulent Transition Prediction on Airfoils -- Unsteady Measurements with the Continuously Rotating DLR-PSP-Model at the Transonic Wind Tunnel Gottingen (DNW-TWG) -- Turbulence Modeling for Reentry-Vehicles -- Computation of the Two-Dimensional Flow in SERN Nozzles -- Experimental Investigation of a Hypersonic Inlet for the TSTO-Configuration ELAC -- Aerodynamic Analysis of the Dual-Mode Ramjet Vehicle JAPHAR -- Study of Shock-Wave/Boundary-Layer Interaction Flowfield on a 24[superscript [degree]] Ramp Model -- Numerical Investigations of Small-Amplitude Disturbances in a Laminar Boundary Layer with Impinging Shock Waves -- Surface Temperature Effects on Shock-Wave Boundary-Layer Interaction of Ramp Flows -- Preliminary Results of Numerical Simulations of Elastic Panels in Transonic Flows -- Numerical Simulation of Laminar Separation-Bubble Control -- On the Structure of Turbulence in the Transition Cylinder Wake -- Investigation of Subgrid-Scale Models in LES of Turbulent Flows with Separation -- Experimental and Numerical Investigations on Transition in a Laminar Separation Bubble -- Boundary-layer Separation Computed by Second-Moment Closure Models -- Experimental Investigation on the Behaviour of Disturbances Emitted from a Point Source in a Laminar Boundary Layer -- Experimental/Numerical Investigation of the Influence of a Pressure Gradient on Acoustic Roughness Receptivity in the Boundary Layer of an Airfoil -- Interference of Wave Trains with Varying Phase Relations in a Decelerated Two-Dimensional Boundary Layer -- Secondary Instability of Steady and Unsteady Crossflow Waves -- Examination of the Eddy-Viscosity Concept Regarding its Physical Justification -- A Numerical Method for Compressible and Low Mach Number Fluid Flow -- Turbulent Two-Dimensional Flow Around a Flexible Membrane Airfoil -- Solution of the Euler Equations on Locally Adaptive B-Spline Grids -- An Algorithm to Treat Flows Bounded by Arbitrarity Shaped Surfaces with Cartesian Meshes -- Grid Refinement Study with a UHCA Wing-Body Configuration Using Richardson Extrapolation and Grid Convergence Index GCI -- Convergence Acceleration on Unstructured Meshes -- Enhancement of a Navier-Stokes Flow Solver for Patched Grids with Non-Coincident Grid Nodes -- Flow and Turbulence Structures in the Wake of a Simplified Car Model (Ahmed Modell) -- Flow Visualisation, Pressure Measurements and Numerical Calculations on Spike-Tipped Bodies -- Tip-Vortices in Transonic Axial-Compressors -- Airframe Noise - Generation and Reduction - a Report on Status and Perspectives of DLR-Research -- Receptivity of Three-Dimensional Boundary Layers to Roughness and Suction - Linear and Nonlinear Effects -- Active Control of Tollmien-Schlichting Instabilities by Multi-Channel Sensor Actuator Systems -- Time Resolved 2D Measurement Techniques for Quantitative Determination of Flow Fields and Surface Pressure Distributions -- Investigation of Transitional Structures in Artificially and Disturbed Excited Flat Plate Boundary Layer Flows Using Stereo and Multi-Plane PIV -- The Meaning of Disturbance Fields in Transition Experiments and Their Detection in the Test Section Flow of a Short Duration Wind Tunnel -- Surface Fence with an Integrated, Piezoresistive Pressure Sensor for Measurements of Static and Dynamic Wall Shear Stress -- Experimental Investigation of the Flow Close to the Surface of a High Lift Airfoil Configuration in a Large Wind Tunnel -- Detection of Density Gradients at Helicopter Rotor Blades in Flight.

Machine converted from AACR2 source record.