New Results in Numerical and Experimental Fluid Mechanics VI: Contributions to the 15th STAB/DGLR Symposium Darmstadt, Germany 2006 (Notes on ... and Multidisciplinary Design, Band 96) - Taschenbuch

EAN (ISBN-13): 9783642093876
ISBN (ISBN-10): 3642093876
Gebundene Ausgabe
Taschenbuch
Erscheinungsjahr: 2010
Herausgeber: Tropea, Cameron, Jakirlic, Suad, Heinemann, Hans-Joachim, Henke, Rolf, Hönlinger, Heinz, Springer
488 Seiten
Gewicht: 0,731 kg
Sprache: eng/Englisch

Buch in der Datenbank seit 2010-05-08T21:01:54+02:00 (Vienna)
Detailseite zuletzt geändert am 2023-11-05T03:11:29+01:00 (Vienna)
ISBN/EAN: 9783642093876

ISBN - alternative Schreibweisen:
3-642-09387-6, 978-3-642-09387-6
Alternative Schreibweisen und verwandte Suchbegriffe:
Autor des Buches: heinemann heinz, rolf heine, henke, jakir, hans heinz, joachim heinz, heinemann edited, hönl, hönlinger, cameron
Titel des Buches: darmstadt, germany 2006, results, the symposium, experimental, ufo symposium, fluid mechanics

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Daten vom Verlag:

Autor/in: Cameron Tropea; Suad Jakirlic; Hans-Joachim Heinemann; Rolf Henke; Heinz Hönlinger
Titel: Notes on Numerical Fluid Mechanics and Multidisciplinary Design; New Results in Numerical and Experimental Fluid Mechanics VI - Contributions to the 15th STAB/DGLR Symposium Darmstadt, Germany 2006
Verlag: Springer; Springer Berlin
474 Seiten
Erscheinungsjahr: 2010-11-25
Berlin; Heidelberg; DE
Gedruckt / Hergestellt in Niederlande.
Sprache: Englisch
213,99 € (DE)
219,99 € (AT)
236,00 CHF (CH)
POD
XIV, 474 p.

BC; Hardcover, Softcover / Technik/Maschinenbau, Fertigungstechnik; Maschinenbau; Verstehen; Aerodynamic Experimental Techniques; Aerodynamic Projects; Aerodynamics; Analytical Methods; Numerical Methods; Schliere; Windtunnels; calculus; fluid mechanics; layers; linear optimization; mechanics; model; numerical analysis; numerics; fluid- and aerodynamics; Mechanical Engineering; Automotive Engineering; Continuum Mechanics; Computational Intelligence; Engineering Fluid Dynamics; Fahrzeugbau; Klassische Mechanik; Künstliche Intelligenz; Maschinenbau: Strömungsmechanik; BB

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 SpatialDiscretization 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 CavityPlaced 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 inInflow System of a Swirl Combustor.
Contributions to the 15. Symposium of the STAB (German Aero-space Aerodynamics Association)