| High Reynolds-number windtunnel testing for the design of Airbus high-lift wings | p. 1 |
| Aerodynamic analysis of flows with low mach- and Reynolds-number under consideration and forecast of transition on the example of a glider | p. 9 |
| Analysis of PIV flow measurements behind the ALVAST-model in high-lift configuration | p. 17 |
| Effect of differential flap settings on the wake vortex evolution of large transport aircraft | p. 25 |
| Investigations on the influence of fins on the extended nearfield of a wing in high-lift configuration | p. 33 |
| Application of the PSP technique in low speed wind tunnels | p. 41 |
| Investigation of tailplane stall for a generic transport aircraft configuration | p. 50 |
| Numerical analysis of transport aircraft using different wing tip devices | p. 59 |
| Aerodynamic optimisation of a flying wing transport aircraft | p. 69 |
| Delta wing steady pressure investigations for sharp and rounded leading edges | p. 77 |
| Computation of delta wing flap oscillations with a Reynolds-averaged Navier-Stokes solver | p. 85 |
| Experimental study on the flowfield of a delta-canard-configuration with deflected leading edge | p. 94 |
| Numerical simulation of maneuvering combat aircraft | p. 103 |
| Experimental investigation on periodic rolling of a delta wing flow at transonic mach numbers | p. 112 |
| Numerical design of a low-noise high-lift system for a supersonic aircraft | p. 120 |
| Chimera simulation of a complete helicopter with rotors as actuator discs | p. 128 |
| Extension of the unstructured TAU-code for rotating flows | p. 136 |
| Unsteady Euler and Navier-Stokes simulations of propellers with the unstructured DLR TAU-code | p. 144 |
| Aerodynamic analysis of jet-blast using CFD considering as example a hangar and an Airbus A380 configuration | p. 152 |
| Flow field study of a supersonic jet exiting into a supersonic stream | p. 160 |
| Behaviour of supersonic overexpanded jets impinging on plates | p. 168 |
| Study of supersonic flow separation induced by a side jet and its control | p. 176 |
| Analytically obtained data compared with shock tunnel heat flux measurements at a conical body at M = 6 | p. 184 |
| Navier-Stokes airfoil computations with automatic transition prediction using the DLR TAU code - a sensitivity study | p. 192 |
| Prediction of attachment line transition for a high-lift wing based on two-dimensional flow calculations with RANS-solver | p. 200 |
| RANS simulation and experiments on the stall behaviour of a tailplane airfoil | p. 208 |
| Experimental and numerical investigations of flow separation and transition to turbulence in an axisymmetric diffuser | p. 217 |
| In-flight and wind tunnel investigations of instabilities on a laminar wing glove | p. 225 |
| Steady three-dimensional streaks and their optimal growth in a laminar separation bubble | p. 233 |
| Applicability and quality of linear stability theory and linear PSE in swept laminar separation bubbles | p. 241 |
| Drag reduction of an Ahmed car model by means of active separation control at the rear vehicle slant | p. 249 |
| Increasing lift by means of active flow control on the flap of a generic high-lift configuration | p. 257 |
| Influencing the mixing process in a turbulent boundary layer by pulsed jet actuators | p. 265 |
| Active flow control by surface smooth plasma actuators | p. 273 |
| Boundary layer influence on supersonic jet/cross-flow interaction in hypersonic flow | p. 281 |
| Numerical rebuilding of a generic body-flap model in an arc heated facility | p. 289 |
| Experimental and numerical investigations of shock/turbulent boundary layer interaction on a double ramp configuration | p. 297 |
| Time accurate simulation of turbulent nozzle flow by the DLR TAU-code | p. 305 |
| Quantitative comparison of measured and numerically simulated erosion rates of SiC based heat shield materials | p. 313 |
| High-end concept to launch micro-satellites into low-Earth-orbit based on combination of a two-stage rocket and a railgun-system | p. 322 |
| Numerical simulation of steady and unsteady aerodynamics of the WIONA (wing with oscillating nacelle) configuration | p. 330 |
| Computation of the flutter boundary of the NLR 7301 airfoil in the transonic range | p. 338 |
| The noise criteria within multidisciplinary high-lift design | p. 348 |
| Effect of noise reducing modifications of the slat on aerodynamic properties of the high-lift system | p. 357 |
| Experimental study on noise reduction through trailing edges brushes | p. 365 |
| A study on trailing edge noise sources using high-speed particle image velocimetry | p. 373 |
| Towards the applicability of the modified von Karman spectrum to predict trailing edge noise | p. 381 |
| Numerical simulation of combustion noise using acoustic perturbation equations | p. 389 |
| Toward efficient solution of the compressible Navier-Stokes equations | p. 397 |
| Direct numerical simulation of a turbulent flow using a spectral/hp element method | p. 405 |
| Numerical simulation of aerodynamic problems with a Reynolds stress turbulence model | p. 413 |
| Efficient large eddy simulation of mach number flow | p. 422 |
| Implementation and usage of structured algorithms within an unstructured CFD-code | p. 430 |
| Numerical flow simulation with moving grids | p. 438 |
| Appropriate turbulence modelling for turbomachinery flows using a two-equation turbulence model | p. 446 |
| Numerical determination of dynamic derivatives for transport aircraft | p. 455 |
| Detached-eddy simulation of the delta wing of a generic aircraft configuration | p. 463 |
| Small disturbance Navier-Stokes equations : application on transonic two-dimensional flows around airfoils | p. 471 |
| Numerical and experimental investigations of turbulent convection with separation in aircraft cabins | p. 479 |
| Investigation of influence of different modelling parameters on calculation of transonic buffet phenomena | p. 487 |
| Anisotropy evolution in relaminarizing turbulent boundary layers : a DNS-aided second-moment closure analysis | p. 496 |
| Turbulent channel flow with periodic hill constrictions | p. 504 |
| Turbulent flow separation control by boundary-layer forcing : a computational study | p. 513 |
| Implementation of propeller simulation techniques at DNW | p. 521 |
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