Beschreibung
InhaltsangabeHigh Aspect-Ratio Wings.- High Reynolds-Number Windtunnel Testing for the Design of Airbus High-Lift Wings.- Aerodynamic Analysis of Flows with Low Mach- and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider.- Analysis of PIV Flow Measurements behind the ALVAST-Model in High-Lift Configuration.- Effect of Differential Flap Settings on the Wake Vortex Evolution of Large Transport Aircraft.- Investigations on the Influence of Fins on the Extended Nearfield of a Wing inHigh-Lift Configuration.- Application of the PSP Technique in Low Speed Wind Tunnels.- Investigation of tailplane stall for a generic transport aircraft configuration.- Numerical analysis of transport aircraft using different wing tip devices.- Aerodynamic Optimisation of a Flying Wing Transport Aircraft.- Low Aspect-Ratio Wings.- Delta Wing Steady Pressure Investigations for Sharp and Rounded Leading Edges.- Computation of Delta Wing Flap Oscillations with a Reynolds-Averaged Navier-Stokes Solver.- Experimental study on the Flowfield of a Delta-Canard-Configuration with Deflected Leading Edge.- Numerical simulation of maneuvering combat aircraft.- Experimental investigation on periodic rolling of a delta wing flow at transonic Mach numbers.- Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft.- Helicopters.- Chimera Simulation of a Complete Helicopter with Rotors as Actuator Discs.- Extension of the Unstructured TAU-Code for Rotating Flows.- Unsteady Euler and Navier-Stokes Simulations of Propellers with the Unstructured DLR TAU-Code.- Aerodynamic Analysis of Jet-Blast using CFD considering as example a Hangar and an AIRBUS A380 configuration.- Bluff Bodies.- Flow Field Study of a Supersonic Jet Exiting into a Supersonic Stream.- Behavior of Supersonic Overexpanded Jets Impinging on Plates.- Study of Supersonic Flow Separation Induced by a Side Jet and its Control.- Analytically obtained data compared with shock tunnel heat flux measurements at a conical body at M = 6.- Laminar Flow Control and Transition.- Navier-Stokes Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code - A Sensitivity Study.- Prediction of attachment line transition for a high-lift wing based on two-dimensional flow calculations with RANS-solver.- RANS Simulation and Experiments on the Stall Behaviour of a Tailplane Airfoil.- Experimental and Numerical Investigations of Flow Separation and Transition to Turbulence in an Axisymmetric Diffuser.- In-Flight and Wind Tunnel Investigalions of Instabilities on a Laminar Wing Glove.- Steady three-dimensional Streaks and their Optimal Growth in a Laminar Separation Bubble.- Applicability and quality of linear stability theory and linear PSE in swept laminar separation bubbles.- Active Flow Control.- Drag Reduction of an Ahmed Car Model by Means of Active Separation Control at the Rear Vehicle Slant.- Increasing Lift by Means of Active Flow Control on the Flap of a Generic High-Lift Configuration.- Influencing the Mixing Process in a Turbulent Boundary Layer by Pulsed Jet Actuators.- Active Flow Control by Surface Smooth Plasma Actuators.- Hypersonic Flows.- Boundary Layer Influence on Supersonic Jet/Cross-Flow Interaction in Hypersonic Flow.- Numerical Rebuilding of a Generic Body-Flap Model in an Arc Heated Facility.- Experimental and Numerical Investigations of Shock/Turbulent Boundary Layer Interaction on a Double Ramp Configuration.- Time Accurate Simulation of Turbulent Nozzle Flow by the DLR TAU-Code.- Quantitative Comparison of Measured and Numerically Simulated Erosion Rates of SiC Based Heat Shield Materials.- High-End Concept to Launch Micro-Satellites into Low-Earth-Orbit based on Combination of a Two-Stage Rocket and a Railgun-System.- Aeroelasticity.- Numerical Simulation of Steady and Unsteady Aerodynamics of the WIONA (Wing with Oscillating Nacelle) Configuration.- Computation of the Flutter Boundary of the NLR 7301 Airfoil in the Transonic Range.-
