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Computational Flight Testing

Results of the Closing Symposium of the German Research Initiative ComFliTe, Braunschweig, Germany, June 11th-12th, 2012

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  • © 2013

Overview

Editors:
  1. Norbert Kroll

    1. , Institute of Aerodynamics and, German Aerospace Center (DLR), Braunschweig, Germany

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  2. Rolf Radespiel

    1. Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

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  3. Jan Willem Burg

    1. Airbus Operations Gmbh, Bremen, Germany

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  4. Kaare Sørensen

    1. Aerodynamics & Methods, Cassidian, Manching, Germany

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  • 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

Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM, volume 123)

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Table of contents (19 chapters)

  1. Front Matter

    Pages 1-7
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  2. AMG in TAU: Adjoint Equations and Mesh Deformation

    • M. Förster, A. Pal
    Pages 1-15

  3. Accurate Simulation of Flows with Convected Vortices: Cartesian TAU

    • Philip Kelleners
    Pages 17-25

  4. Hybrid RANS-LES Models

    • Koen Geurts, Axel Probst
    Pages 27-41

  5. Investigation of the Resolution Requirements for a Hybrid RANS/LES Simulation of a Multi-element Airfoil

    • S. Reuß, T. Knopp, D. Schwamborn
    Pages 43-57

  6. Improved Transition and Reynolds Stress Modeling in RANS Simulations

    • René-Daniel Cécora, Rolf Radespiel, Axel Probst
    Pages 59-74

  7. Simulation of Maximum Lift Using URANS for a High-Lift Transport Configuration

    • J. W. van der Burg, M. Luehmann
    Pages 75-88

  8. Industrialization of the Automatic Transition Prediction in the DLR TAU Code

    • Normann Krimmelbein
    Pages 89-98

  9. Variable-Fidelity and Reduced-Order Models for Aero Data for Loads Predictions

    • Stefan Görtz, Ralf Zimmermann, Zhong-Hua Han
    Pages 99-112

  10. Response Surface Methods for Efficient Aerodynamic Surrogate Models

    • Benjamin Rosenbaum, Volker Schulz
    Pages 113-129

  11. Nonlinear Reduced Order Modeling for Aeroelastic Simulation with Neural Networks

    • K. Lindhorst, M. C. Haupt, P. Horst
    Pages 131-149

  12. Projection-Based Model Order Reduction for Steady Aerodynamics

    • Alexander Vendl, Heike Faßbender
    Pages 151-166

  13. Implementation of an Automatic Multi-fidelity Scheme for Industrial Applications in the Cassidian SimServer Environment

    • Kurt Sermeus, Luca Nardin, Kaare A. Sørensen
    Pages 167-181

  14. Modeling of Movable Control Surfaces and Atmospheric Effects

    • Lars Reimer, Ralf Heinrich
    Pages 183-206

  15. Coupling Strategies for Large Industrial Models

    • Jens Neumann, Wolf Krüger
    Pages 207-222

  16. NASTRAN Based Static CFD-CSM Coupling in FlowSimulator

    • Bernd Stickan, Hans Bleecke, Silvio Schulze
    Pages 223-234

  17. DLR Pilot Applications in ComFliTe

    • Ralf Heinrich, Lars Reimer, Andreas Michler, Britta Ernst, Markus Ritter, Jens Neumann
    Pages 235-247

  18. Industrial ComFliTe Applications

    • Hans Bleecke, Bernd Stickan
    Pages 249-256

  19. Multi-component Modeling with the Dual Mesh Connect Approach

    • Kaare A. Sørensen
    Pages 257-271

  20. Transonic Tail Buffet Simulations on the ATRA Research Aircraft

    • Sebastian A. Illi, Thorsten Lutz, Ewald Krämer
    Pages 273-287
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Keywords

About this book

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.

Editors and Affiliations

  • , Institute of Aerodynamics and, German Aerospace Center (DLR), Braunschweig, Germany

    Norbert Kroll

  • Institute of Fluid Mechanics, Technische Universität Braunschweig, Braunschweig, Germany

    Rolf Radespiel

  • Airbus Operations Gmbh, Bremen, Germany

    Jan Willem Burg

  • Aerodynamics & Methods, Cassidian, Manching, Germany

    Kaare Sørensen

Bibliographic Information

  • 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: Norbert Kroll, Rolf Radespiel, Jan Willem Burg, Kaare Sørensen

  • Series Title: Notes on Numerical Fluid Mechanics and Multidisciplinary Design

  • DOI: https://doi.org/10.1007/978-3-642-38877-4

  • Publisher: Springer Berlin, Heidelberg

  • eBook Packages: Engineering, Engineering (R0)

  • Copyright Information: Springer-Verlag Berlin Heidelberg 2013

  • Hardcover ISBN: 978-3-642-38876-7Published: 01 July 2013

  • Softcover ISBN: 978-3-662-51106-0Published: 27 August 2016

  • eBook ISBN: 978-3-642-38877-4Published: 18 June 2013

  • Series ISSN: 1612-2909

  • Series E-ISSN: 1860-0824

  • Edition Number: 1

  • Number of Pages: VIII, 289

  • Number of Illustrations: 100 b/w illustrations, 92 illustrations in colour

  • Topics: Aerospace Technology and Astronautics, Fluid- and Aerodynamics, Engineering Fluid Dynamics

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