Computational Flight Testing
Results of the Closing Symposium of the German Research Initiative ComFliTe, Braunschweig, Germany, June 11th-12th, 2012
Seiten
2016
|
1. Softcover reprint of the original 1st ed. 2013
Springer Berlin (Verlag)
978-3-662-51106-0 (ISBN)
Springer Berlin (Verlag)
978-3-662-51106-0 (ISBN)
This book reports on the ComFliTe research initiative to enhance numerical simulation of flight physics. Covers improved physical modeling, more efficient handling of aircraft control surfaces and better simulation of flight maneuvers like gust encounter.
This book reports on the German research initiative ComFliTe (Computational Flight Testing), the main goal of which was to enhance the capabilities of and tools for numerical simulation in flight physics to support future aircraft design and development. The initiative was coordinated by the German Aerospace Center (DLR) and promoted collaboration between the aircraft industry and academia. Activities focused on improving physical modeling for separated flows, developing advanced numerical algorithms for series computations and sensitivity predictions, as well as surrogate and reduced order modeling for aero data production and developing robust fluid-, structure- and flight mechanics coupling procedures. Further topics included more efficient handling of aircraft control surfaces and improving simulation methods for maneuvers, such as gust encounter. The important results of this three-year initiative were presented during the ComFliTe closing symposium, which took place at the DLR in Braunschweig, Germany, on 11-12 June 2012. Computational Flight Testing addresses both students and researchers in the areas of mathematics, numerical simulation and optimization methods, as well as professionals in aircraft design working at the forefront of their field.
This book reports on the German research initiative ComFliTe (Computational Flight Testing), the main goal of which was to enhance the capabilities of and tools for numerical simulation in flight physics to support future aircraft design and development. The initiative was coordinated by the German Aerospace Center (DLR) and promoted collaboration between the aircraft industry and academia. Activities focused on improving physical modeling for separated flows, developing advanced numerical algorithms for series computations and sensitivity predictions, as well as surrogate and reduced order modeling for aero data production and developing robust fluid-, structure- and flight mechanics coupling procedures. Further topics included more efficient handling of aircraft control surfaces and improving simulation methods for maneuvers, such as gust encounter. The important results of this three-year initiative were presented during the ComFliTe closing symposium, which took place at the DLR in Braunschweig, Germany, on 11-12 June 2012. Computational Flight Testing addresses both students and researchers in the areas of mathematics, numerical simulation and optimization methods, as well as professionals in aircraft design working at the forefront of their field.
Innovative Algorithms.- Turbulence and Transition Modeling.- Surrogate Modelling.- Multidisciplinary Analysis.- Industrial Applications.
| Erscheinungsdatum | 02.09.2016 |
|---|---|
| Reihe/Serie | Notes on Numerical Fluid Mechanics and Multidisciplinary Design |
| Zusatzinfo | VIII, 289 p. 192 illus., 92 illus. in color. |
| Verlagsort | Berlin |
| Sprache | englisch |
| Maße | 155 x 235 mm |
| Themenwelt | Technik ► Luft- / Raumfahrttechnik |
| Schlagworte | Aerospace and aviation technology • Aerospace Technology and Astronautics • astronautics • Coupling Strategies for Large Industrial CFD/CSM M • Coupling Strategies for Large Industrial CFD/CSM Models • Efficient Solution Algorithms for Adjoint Solvers • Engineering • engineering fluid dynamics • fluid- and aerodynamics • fluid mechanics • Mechanics of Fluids • Mesh Deformation • Modelling of Movable Control Surfaces • Multidisciplinary Analysis • Reynolds Stress Models, Hybrid RANS/LES • Simulation of Aircraft Manoeuvres • Simulation of Thrust Reverser • Surrogate Modelling • Turbulence and Transition Modelling |
| ISBN-10 | 3-662-51106-1 / 3662511061 |
| ISBN-13 | 978-3-662-51106-0 / 9783662511060 |
| Zustand | Neuware |
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