Computational Flight Testing
Results of the Closing Symposium of the German Research Initiative ComFliTe, Braunschweig, Germany, June 11th-12th, 2012
Editors: Kroll, N., Radespiel, R., van der Burg, J.W., Sorensen, K. (Eds.)
Free Preview- Results form the German research initiative ComFliTe (Computational Flight Testing)
- Advanced research in multidisciplinary numerical simulation in flight physics and their applications within the aeronautical industry
- Written by leading experts in the field
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- About this book
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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.
- Table of contents (19 chapters)
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AMG in TAU: Adjoint Equations and Mesh Deformation
Pages 1-15
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Accurate Simulation of Flows with Convected Vortices: Cartesian TAU
Pages 17-25
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Hybrid RANS-LES Models
Pages 27-41
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Investigation of the Resolution Requirements for a Hybrid RANS/LES Simulation of a Multi-element Airfoil
Pages 43-57
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Improved Transition and Reynolds Stress Modeling in RANS Simulations
Pages 59-74
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Table of contents (19 chapters)
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Bibliographic Information
- Bibliographic Information
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- Book Title
- Computational Flight Testing
- Book Subtitle
- Results of the Closing Symposium of the German Research Initiative ComFliTe, Braunschweig, Germany, June 11th-12th, 2012
- Editors
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- Norbert Kroll
- Rolf Radespiel
- Jan Willem van der Burg
- Kaare Sorensen
- Series Title
- Notes on Numerical Fluid Mechanics and Multidisciplinary Design
- Series Volume
- 123
- Copyright
- 2013
- Publisher
- Springer-Verlag Berlin Heidelberg
- Copyright Holder
- Springer-Verlag Berlin Heidelberg
- eBook ISBN
- 978-3-642-38877-4
- DOI
- 10.1007/978-3-642-38877-4
- Hardcover ISBN
- 978-3-642-38876-7
- Softcover ISBN
- 978-3-662-51106-0
- Series ISSN
- 1612-2909
- Edition Number
- 1
- Number of Pages
- VIII, 289
- Number of Illustrations
- 100 b/w illustrations, 92 illustrations in colour
- Topics
