MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design Results of the closing symposium of the MEGADESIGN and MegaOpt projects, Braunschweig, Germany, May 23 and 24, 2007 /

MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design Results of the closing symposium of the MEGADESIGN and MegaOpt projects, Braunschweig, Germany, May 23 and 24, 2007 /

Detalles Bibliográficos
Autor Corporativo: SpringerLink (Online service)
Otros Autores: Kroll, Norbert. (Editor ), Schwamborn, Dieter. (Editor ), Becker, Klaus. (Editor ), Rieger, Herbert. (Editor ), Thiele, Frank. (Editor )
Formato: eBook
Lenguaje:English
Publicado: Berlin, Heidelberg : Springer Berlin Heidelberg : Imprint: Springer, 2009.
Edición:1st ed. 2009.
Colección:Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107
Materias:
Aerospace engineering.
Astronautics.
Continuum physics.
Algebra.
Fluid mechanics.
Applied mathematics.
Engineering mathematics.
Engineering design.
Aerospace Technology and Astronautics.
Classical and Continuum Physics.
Engineering Fluid Dynamics.
Mathematical and Computational Engineering.
Engineering Design.
Acceso en línea:https://doi.org/10.1007/978-3-642-04093-1
Tabla de Contenidos:
  • 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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