New Results in Numerical and Experimental Fluid Mechanics III: Contributions to the 12th STAB/DGLR Symposium Stuttgart, Germany 2000

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Siegfried Wagner, Ulrich Rist, Hans-Joachim Heinemann, Reinhard Hilbig
Springer Science & Business Media, Feb 26, 2002 - Technology & Engineering - 436 pages
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This volume contains the papers of a German symposium dealing with research and project work in numerical and experimental aerodynamics and fluidmechanics for aerospace and other applications. It gives a broad overview over the ongoing work in this field in Germany.

 

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Contents

Design Work for the A3XX HighLiftWing
3
Recent Improvements in the Measurement of Aerodynamic Damping Derivatives
11
Calculation of Horizontal Stabilizer Efficiency with a NavierStokes Code
19
3D RANS Simulations for HighLift Analysis of Transport Aircraft Configurations
27
Numerical Investigation of the ReynoldsNumberEffect on the Setting Sensitivity of a 2D HighLift MultiElement Airfoil
35
Separation Control on a HighLift Configuration by Periodic Exitation
42
Numerical Investigation of the Effect of the HighLift Configuration of a Transport Aircraft on its Vortex Wake
50
The Relationship Between Near andFarField of Vortex Wakes from Aircraft with High Aspect Ratio Wings
58
Experimental Investigation on the Behaviour of Disturbances Emitted from a Point Source in a Laminar Boundary Layer
223
of a Pressure Gradient on Acoustic Roughness Receptivity in the Boundary Layer of an Airfoil
231
Interference of Wave Trains with Varying Phase Relations in a Decelerated TwoDimensional Boundary Layer
239
Secondary Instability of Steady and Unsteady Crossflow Waves
247
Examination of the EddyViscosity Concept Regarding its Physical Justification
255
Mathematical Fundamentals Numerical Simulation
263
A Numerical Method for Compressible and Low Mach Number Fluid Flow
265
Turbulent TwoDimensional Flow Around a Flexible Membrane Airfoil
273

Influence of Different Flap Settings on the Hazard Posed to Following Aircraft
66
Numerical Simulation of WakeVortex Encounters Using the ChimeraTechnique
74
Aspects of Low Speed Wind Tunnel Testing on an A400M Model with Propeller Simulation
82
Coupling of DLR NavierStokes Solver FLOWer with an eNDatabase Method for LaminarTurbulent Transition
92
Low AspectRatio Wings
101
Unsteady Measurements with the Continuously Rotating DLRPSPModel at the Transonic Wind Tunnel Gottingen DNWTWG
103
Hypersonic Flows
111
Turbulence Modeling for ReentryVehicles
113
Computation of the TwoDimensional Flow in SERN Nozzles
121
Experimental Investigation of a Hypersonic Inlet for the TSTOConfiguration ELAC
129
JAPHAR
137
Study of ShockWaveBoundaryLayer Interaction Flowfield on a 24 Ramp Model
145
Disturbances in a Laminar Boundary Layer with Impinging Shock Waves
153
Surface Temperature Effects on ShockWave BoundaryLayer Interaction of Ramp Flows
161
FluidStructureCoupling
169
Preliminary Results of Numerical Simulations of Elastic Panels in Transonic Flows
171
Fundamentals of Fluid Flow
179
Numerical Simulation of Laminar SeparationBubble Control
181
On the Structure of Turbulence in the Transition Cylinder Wake
189
Transition and Fluidmechanical Modelling
197
Investigation of SubgridScale Models in LES of Turbulent Flows with Separation
199
Experimental and Numerical Investigations on Transition in a Laminar Separation Bubble
207
Boundarylayer Separation Computed by SecondMoment Closure Models
215
Solution of the Euler Equations on Locally Adaptive BSpline Grids
281
An Algorithm to Treat Flows Bounded by Arbitrarily Shaped Surfaces with Cartesian Meshes
289
Configuration Using Richardson Extrapolation and Grid Convergence Index GCI
297
Convergence Acceleration on Unstructured Meshes
304
Enhancement of a NavierStokes Flow Solver for Patched Grids with NonCoincident Grid Nodes
312
Bluff Bodies
321
Flow and Turbulence Structures in the Wake of a Simplified Car Model Ahmed Modell
323
Flow Visualisation Pressure Measurements and Numerical Calculations on SpikeTipped Bodies
331
Turbomachineri
339
TipVortices in Transonic AxialCompressors
341
Airframe Noise
351
Airframe Noise Generation and Reduction A Report on Status and Perspectives of DLRResearch
353
Laminar Flow Control
365
Receptivity of ThreeDimensional Boundary Layers to Roughness and Suction Linear and Nonlinear Effects
367
Active Control of TollmienSchlichting Instabilities by MultiChannel Sensor Actuator Systems
375
Measuring Techniques
383
for Quantitative Determination of Flow Fields and Surface Pressure Distributions
385
and Disturbed Excited Flat Plate Boundary Layer Flows Using Stereo and MultiPlane PIV
395
and Their Detection in the Test Section Flow of a Short Duration Wind Tunnel
403
Sensor for Measurements of Static and Dynamic Wall Shear Stress
411
Experimental Investigation of the Flow Close to the Surface of a High Lift Airfoil Configuration in a Large Wind Tunnel
419
Detection of Density Gradients at Helicopter Rotor Blades in Flight
426
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