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07172nam a22004335i 4500 |
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978-3-540-74460-3 |
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20191021213747.0 |
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cr nn 008mamaa |
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100301s2008 gw | s |||| 0|eng d |
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|a 9783540744603
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|a 10.1007/978-3-540-74460-3
|2 doi
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|a Sistema de Bibliotecas del Tecnológico de Costa Rica
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|a New Results in Numerical and Experimental Fluid Mechanics VI
|b Contributions to the 15th STAB/DGLR Symposium Darmstadt, Germany 2006 /
|c edited by Cameron Tropea, Suad Jakirlic, Hans-Joachim Heinemann, Rolf Henke, Heinz Hönlinger.
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|a 1st ed. 2008.
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|a Berlin, Heidelberg :
|b Springer Berlin Heidelberg :
|b Imprint: Springer,
|c 2008.
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| 300 |
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|a XIV, 474 p.
|b online resource.
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| 336 |
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|a text
|b txt
|2 rdacontent
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|a computer
|b c
|2 rdamedia
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|a online resource
|b cr
|2 rdacarrier
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|a Notes on Numerical Fluid Mechanics and Multidisciplinary Design,
|v 96
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|a 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.
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| 650 |
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|a Mechanical engineering.
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| 650 |
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|a Automotive engineering.
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| 650 |
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0 |
|a Fluids.
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| 650 |
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|a Computational intelligence.
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| 650 |
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|a Fluid mechanics.
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| 650 |
1 |
4 |
|a Mechanical Engineering.
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| 650 |
2 |
4 |
|a Automotive Engineering.
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| 650 |
2 |
4 |
|a Fluid- and Aerodynamics.
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| 650 |
2 |
4 |
|a Computational Intelligence.
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| 650 |
2 |
4 |
|a Engineering Fluid Dynamics.
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| 700 |
1 |
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|a Tropea, Cameron.
|e editor.
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| 700 |
1 |
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|a Jakirlic, Suad.
|e editor.
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| 700 |
1 |
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|a Heinemann, Hans-Joachim.
|e editor.
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| 700 |
1 |
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|a Henke, Rolf.
|e editor.
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| 700 |
1 |
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|a Hönlinger, Heinz.
|e editor.
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| 710 |
2 |
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|a SpringerLink (Online service)
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| 773 |
0 |
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|t Springer eBooks
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| 856 |
4 |
0 |
|u https://doi.org/10.1007/978-3-540-74460-3
|