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03615nam a22004815i 4500 |
| 001 |
978-3-642-04093-1 |
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20191021192552.0 |
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cr nn 008mamaa |
| 008 |
100301s2009 gw | s |||| 0|eng d |
| 020 |
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|a 9783642040931
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| 024 |
7 |
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|a 10.1007/978-3-642-04093-1
|2 doi
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| 040 |
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|a Sistema de Bibliotecas del Tecnológico de Costa Rica
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| 245 |
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|a MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design
|b Results of the closing symposium of the MEGADESIGN and MegaOpt projects, Braunschweig, Germany, May 23 and 24, 2007 /
|c edited by Norbert Kroll, Dieter Schwamborn, Klaus Becker, Herbert Rieger, Frank Thiele.
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| 250 |
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|a 1st ed. 2009.
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| 260 |
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|a Berlin, Heidelberg :
|b Springer Berlin Heidelberg :
|b Imprint: Springer,
|c 2009.
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| 300 |
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|a XI, 313 p.
|b online resource.
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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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 107
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| 505 |
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|a Reduction of Simulation Time -- Recent Developments of TAU Adaptation Capability -- Adaptive Wall Function for the Prediction of Turbulent Flows -- Acceleration of CFD Processes for Transport Aircraft -- Efficient Combat Aircraft Simulations with the TAU RANS Code -- Improvement of Simulation Quality -- Universal Wall Functions for Aerodynamic Flows: Turbulence Model Consistent Design, Potential and Limitations -- Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models -- Transition Prediction for Three-Dimensional Configurations -- Application of Transition Prediction -- Numerical Simulation Quality Assessment for Transport Aircraft -- Fluid Structure Coupling -- Computational Methods for Aero-Structural Analysis and Optimisation of Aircrafts Based on Reduced-Order Structural Models -- Development and Application of TAU-ANSYS Coupling Procedure -- Fluid-Structure Coupling: Simplified Structural Model on Complex Configurations -- Improvement of Shape Optimization Strategies -- Development of an Automated Artificial Neural Network for Numerical Optimization -- modeFRONTIER©, a Framework for the Optimization of Military Aircraft Configurations -- One-Shot Methods for Aerodynamic Shape Optimization -- Automatic Differentiation of FLOWer and MUGRIDO -- Adjoint Methods for Coupled CFD-CSM Optimization -- Aerodynamic and Multidisciplinary Optimization of 3D-Configurations -- Aerodynamic Optimization for Cruise and High-Lift Configurations -- Aerodynamic Optimization of an UCAV Configuration -- Flexible Wing Optimisation Based on Shapes and Structures -- Multidisciplinary Optimization of an UAV Combining CFD and CSM.
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| 650 |
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|a Aerospace engineering.
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| 650 |
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0 |
|a Astronautics.
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| 650 |
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0 |
|a Continuum physics.
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| 650 |
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0 |
|a Algebra.
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| 650 |
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0 |
|a Fluid mechanics.
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| 650 |
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0 |
|a Applied mathematics.
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| 650 |
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0 |
|a Engineering mathematics.
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| 650 |
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0 |
|a Engineering design.
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| 650 |
1 |
4 |
|a Aerospace Technology and Astronautics.
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| 650 |
2 |
4 |
|a Classical and Continuum Physics.
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| 650 |
2 |
4 |
|a Algebra.
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| 650 |
2 |
4 |
|a Engineering Fluid Dynamics.
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| 650 |
2 |
4 |
|a Mathematical and Computational Engineering.
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| 650 |
2 |
4 |
|a Engineering Design.
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| 700 |
1 |
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|a Kroll, Norbert.
|e editor.
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| 700 |
1 |
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|a Schwamborn, Dieter.
|e editor.
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| 700 |
1 |
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|a Becker, Klaus.
|e editor.
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| 700 |
1 |
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|a Rieger, Herbert.
|e editor.
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| 700 |
1 |
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|a Thiele, Frank.
|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/10.1007/978-3-642-04093-1
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