New Results in Numerical and Experimental Fluid Mechanics VI Contributions to the 15th STAB/DGLR Symposium Darmstadt, Germany 2006 /
| Autor Corporativo: | |
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| Otros Autores: | , , , , |
| Formato: | eBook |
| Lenguaje: | English |
| Publicado: |
Berlin, Heidelberg :
Springer Berlin Heidelberg : Imprint: Springer,
2008.
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| Edición: | 1st ed. 2008. |
| Colección: | Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
96 |
| Materias: | |
| Acceso en línea: | https://doi.org/10.1007/978-3-540-74460-3 |
Tabla de Contenidos:
- Airplane Acrodynamics
- An Airbrake Design Methodology for Steep Approaches
- High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Properties
- Numerical Analysis of Wing Vortices
- Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Model
- URANS and DES Simulation of Flow Around a Rectangular Cylinder
- Active Manipulation of a Rectangular Wing Vortex Wake with Oscillating Ailerons and Winglet-Integrated Rudders
- A New Actuator Disk Model for the TAU Code and Application to a Sailplaine with a Folding Engine
- Design of a Retrofit Winglet for a Transport Aircraft with Assessment of Cruise and Ultimate Structural Loads
- Flow Control
- Numerical Simulation of a Wing with a Gapless High-Lift System Using Circulation Control
- Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow
- A Flat Plate Experiment for Investigations of Vortex Generator Jets at High Reynolds Number
- Experimental Simulation and Test Techniques
- Measurement of Unsteady Surface Forces by Means of Piezoelectrical Copolymer Coatings
- Studies of Reynolds Number Effects on Wing Tip Vortex Positions by Means of Laser Light Sheet (LLS) and Background Oriented Schlieren (BOS) Technique Under Cryogenic Conditions
- Project ForMEx — A New CFD Approach for Transposition of Wind Tunnel Data Towards Flight Conditions
- Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio Circular Cylinder Mounted on a Ground Plate
- An Investigation into Internal and External Force Balance Configurations for Short Duration Wind Tunnels
- Numerics
- Multiple Discipline Take-Off Weight Minimization for a Supersonic Transport Aircraft
- Three-Dimensional Discontinuous Galerkin Codes to Simulate Viscous Flow by Spatial Discretization of High Order and Curved Elements on Unstructured Grids
- The Space-Time Expansion DG Method
- The Parallel Mesh Deformation of the DLR TAU-Code
- Simulation of Oscillating Airfoils and Moving Flaps Employing the DLR-TAU Unsteady Grid Adaptation
- RANS Simulations with One and Six Degrees of Freedom Rigid Body Motions
- Improvement of the Automatic Grid Adaptation for Vortex Dominated Flows Using Advanced Vortex Indicators with the DLR-Tau Code
- Adjoint Algorithms for the Optimization of 3d Turbulent Configurations
- Enhanced Runge-Kutta/Implicit Methods for Solving the Navier-Stokes Equations
- Laminar Flow Control and Transition
- Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction Using the DLR TAU Code
- Manipulation of Attachment Line Transition by Geometry Modification at the Slat of a Multi-element Airfoil
- Using CryoTSP as a Tool for Transition Detection and Instability Examination at High Reynolds Numbers
- Direct Numerical Simulation of a Short Laminar Separation Bubble and Early Stages of the Bursting Process
- Experimental Investigations of Controlled Transition in a Laminar Separation Bubble at an Axisymmetric Diffuser
- Development of a Sensor-Actuator-System for Active Control of Boundary Layer Instabilities in Compressible Flows
- Evaluation of Initial Amplitudes of Free-Stream Excited Tollmien-Schlichting Waves from Flight-Test Data
- The Role of Turbulent Dissipation for Flow Control of Near-Wall Turbulence
- Hypersonic Flows
- Radical Farming in Scramjets
- Aerothermodynamic Investigation of the Pre-X Configuration in HEG
- SHEFEX — A First Aerodynamic Post-flight Analysis
- Simulation of Magnetohydrodynamic Effects on an Ionised Hypersonic Flow by Using the TAU Code
- Heat Fluxes Inside a Cavity Placed at the Nose of a Projectile Measured in a Shock Tunnel at Mach 4.5
- Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6
- Turbomachines
- Control of Flow Separation in Adverse Pressure Gradients by Means of Crosswise Grooved Surfaces for Turbo Machine Applications
- Wave Drag Reduction Approach for Lattice Wings at High Speeds
- Forces and Velocity Measurements in Ship Propulsion Systems
- Flow Past Bodies
- Numerical Simulation of the Flow Around a Finite Cylinder with Ground Plate in Comparison to Experimental Measurements
- Numerical Simulation of Aerodynamic Problems with the SSG/LRR-? Reynolds Stress Turbulence Model Using the Unstructured TAU Code
- Numerical Simulation of the Flow Field Around the Stratospheric Observatory for Infrared Astronomy
- Large Eddy Simulation / Direct Numerical Simulation
- DNS of Compressible Inert and Infinitely Fast Reacting Mixing Layers
- Developement of a Numerical Procedure for Direct Simulations of Turbulent Convection in a Closed Rectangular Cell
- Computation of Supersonic Base Flow Using Detached Eddy Simulation
- Large-Eddy Simulation of Tundish Flows Using Preconditioning
- Numerical Investigations of Effusion Cooling in Hypersonic Boundary-Layer Flow
- Aeroacoustics
- Numerical Investigation of Flow-Induced Noise Generation at the Nozzle End of Jet Engines
- Numerical Analysis of Sound Generating Mechanisms of a High-Lift Device
- On the Design of Silent Trailing-Edges
- Investigation of Flow Induced Sound Radiated by a Forward Facing Step
- Miscellaneous
- Application of PIV Techniques for Rotor Blade Tip Vortex Characterization
- Automatic Differentiation of an Entire Design Chain for Aerodynamic Shape Optimization
- Computational Study of Mean Flow and Turbulence Structure in Inflow System of a Swirl Combustor.