ISBN: 3540426965
TITLE: New Results in Numerical and Experimental Fluid Mechanics III
AUTHOR: Wagner et al. (Hrsg.)
TOC:

High Aspect-Ratio Wings
D. RECKZEH: Design Work for the A3XX High-Lift-Wing 3
A.-R. HBNER, T. LSER: Recent Improvements in the Measurement of Aerodynamic Damping Derivatives 11
C. NEBEL, D. HUMMEL: Calculation of Horizontal Stabilizer Efficiency with a Navier-Stokes Code 19
S. MELBER: 3D RANS Simulations for High-Lift Analysis of Transport Aircraft Configurations 27
J. WILD: Numerical Investigation of the Reynolds-Number-Effect on the Setting Sensitivity of a 2D High-Lift Multi-Element Airfoil 35
F. TINAPP, W. NITSCHE: Separation Control on a High-Lift Configuration by Periodic Exitation 42
E. STUMPF: Numerical Investigation of the Effect of the High-Lift Configuration of a Transport Aircraft on its Vortex Wake 50
R. STUFF: The Relationship Between Near- and-Far-Field of Vortex Wakes from Aircraft with High Aspect Ratio Wings 58
1. SCHELL, E. ZGER, D. JACOB: Influence of Different Flap Settings on the Hazard Posed to Following Aircraft 66
R. HEINRICH: Numerical Simulation of Wake-Vortex Encounters Using the Chimera-Technique 74
M. HUHND, S. SCHMID-GLLER: Aspects of Low Speed Wind Tunnel Testing on an A400M Model with Propeller Simulation 82
A. KRUMBEIN: Coupling of DLR Navier-Stokes Solver FLOWer with an e^N-Database Method for Laminar-Turbulent Transition Prediction on Airfoils 92
Low Aspect-Ratio Wings
M. BRUSE, K.-W. BOCK, TUSCHE, M. JACOBS: Unsteady Measurements with the Continuously Rotating DLR-PSP-Model at the Transonic Wind Tunnel Gttingen (DNW-TWG) 103
Hypersonic Flows
C. WEBER, R. BEHR, C. WEILAND: Turbulente Modeling for Reentry-Vehicles 113
T. LINK, W.W. KOSCHEL: Computation of the Two-Dimensional Flow in SERN Nozzles 121
N. NEUBACHER, A. HENCKELS, T. GAWEHN: Experimental Investigation of a Hypersonic Inlet for the TSTO-Configuration ELAC 129
T. EGGERS: Aerodynamic Analysis of the Dual-Mode Ramjet Vehicle JAPHAR 137
SB. VERMA, G. KOPPENWALLNER: Study of Shock-Wave/Boundary-Layer Interaction Flowfield on a 24" Ramp Model 145
A. PAGELLA, U. RIST, S. WAGNER: Numerical Investigations of Small-Amplitude Disturbances in a Laminar Boundary Layer with Impinging Shock Waves 153
M. BLEILEBENS, H. OLIVIER: Surface Temperature Effects on Shock-Wave Boundary-Layer Interaction of Ramp Flows 161
Fluid-Structure-Coupling
J. HURKA, J. BALLMANN: Preliminary Results of Numerical Simulations of Elastic Panels in Transonic Flows 171
Fundamentals of Fluid Flow
U. RIST, K. AUGUSTIN, S. WAGNER: Numerical Simulation of Laminar Separation-Bubble Control 181
M. BREDE, A. LEDER: On the Structure of Turbulence in the Transition Cylinder Wake 189
Transition and Fluidmechanical Modelling
S. SCHMIDT, F. THIELE: Investigation of Subgrid-Scale Models in LES of Turbulent Flows with Separation 199
M. LANG, O. MARXEN, U. RIST, S. WAGNER: Experimental and Numerical Investigations on Transition in a Laminar Separation Bubble 207
S. JAKIRLIC, I. HADZIC, A. DJUGUM, C. TROPEA: Boundary-layer Separation Computed by Second-Moment Closure Models 215
J. FREY, R. BUCKISCH, L. MLLER, R. GRUNDMANN: Experimental Investigation on the Behaviour of Disturbances Emitted from a Point Source in a Laminar Boundary Layer 223
S. HERR, A. WRNER, W. WURZ, U. RIST, S. WAGNER: Experimental/Numerical Investigation of the Influence of a Pressure Gradient on Acoustic Roughness Receptivity in the Boundary Layer of an Airfoil 231
C. STEMMER, M. KLOKER: Interference of Wave Trains with Varying Phase Relations in a Decelerated Two-Dimensional Boundary Layer 239
P. WASSERMANN, M. KLOKER, S. WAGNER: Secondary Instability of Steady and Unsteady Crossflow Waves 247
H. FRAHNERT, U.CH. DALLMANN: Examination of the Eddy-Viscosity Concept Regarding its Physical Justification 255
Mathematical Fundamentals / Numerical Simulation
A. MEISTER: A Numerical Method for Compressible and Low Mach Number Fluid Flow 265
U. BUNGE, T. RUNG, F. THIELE: Turbulent Two-Dimensional Flow Around a Flexible Membrane Airfoil 273
F. BRAMKAMP, J. BALLMANN: Solution of the Euler Equations on Locally Adaptive B-Spline Grids 281
F. TREMBLAY, R. FRIEDRICH: An Algorithm to Treat Flows Bounded by Arbitrarily Shaped Surfaces with Cartesian Meshes 289
M. RAKOWITZ: Grid Refinement Study with a UHCA Wing-Body Configuration Using Richardson Extrapolation and Grid Convergence Index GCI 297
C.-C. ROSSOW: Convergence Acceleration on Unstructured Meshes 304
T. SCHWARZ: Enhancement of a Navier-Stokes Flow Solver for Patched Grids with Non-Coincident Grid Nodes 312
Bluff Bodies
H. LIENHART, C. STOOTS, S. BECKER: Flow and Turbulence Structures in the Wake of a Simplified Car Model (Ahmed Modell) 323
J. SRULIJES, P. GNEMMI, K. RUNNE, F. SEILER: Flow Visualisation, Pressure Measurements and Numerical Calculations on Spike-Tipped Bodies 331
Turbomachineri
W. HOFMANN, J. BALLMANN: Tip-Vortices in Transonic Axial-Compressors 341
Airframe Noise
W. DOBRZYNSIU, H. HELLER, J. DELFS: Airframe Noise - Generation and Reduction - a Report on Status and Perspectives of DLR-Research 353
Laminar Flow Control
E. JANKE: Receptivity of Three-Dimensional Boundary Layers to Roughness and Suction - Linear and Nonlinear Effects 367
D. STURZEBECHER, W. NITSCHE: Active Control of Tolhnien-Schlichting Instabilities by Multi-Channel Sensor Actuator Systems 375
Measuring Techniques
K.-A. BTEFISCH: Time Resolved 2D Measurement Techniques for Quantitative Determination of Flow Fields and Surface Pressure Distributions 385
A. SCHRDER, J. KOMPENHANS: Investigation of Transitional Structures in Artificially and Disturbed Excited Flat Plate Boundary Layer Flows Using Stereo and Multi-Plane PIV 395
U. GAISBAUER, H. KNAUSS, S. WAGNER, J. WEISS: The Meaning of Disturbance Fields in Trasition Experiments and Their Detection in the Test Section Flow of a Short Duration Wind Tunnel 403
O. BURKHARDT, U.G.S. DINATA, W. NITSCHE: Surface Fence with an Integrated, Piezoresistive Pressure Sensor for Measurements of Static and Dynamic Wall Shear Stress 411
T.J. MLLER, A. BERGMANN: Experimental Investigation of the Flow Close to the Surface of a High Lift Airfoil Configuration in a Large Wind Tunnel 419
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