AeroStruct: Enable and Learn How to Integrate Flexibility in Design

Part I. Use-Case FORSwing

1. Integrated Process Chain for Aerostructural Wing Optimization and Application to an NLF Forward Swept Composite Wing
Tobias Wunderlich, Lars Reimer

2. Automated Structural Design of Composite Forward Swept Wings
Sascha Dähne, Lars Heinrich

3. Design Procedure for Optimum Fiber Composite Airframe Structures Within an Automated Multidisciplinary Design and Optimization Process
Michael Seibel

4. Development of Flight Control Functions forIntegration in Gust Load Simulations
Alexander Hamann

Part II. Use-Case FlexCraft

5. Introduction to Airbus Use-Case “FlexCraft”
Frank Theurich, Klaus Becker

6. On Recent Advances in Industrial High-Fidelity Aeroelasticity
Bernd Stickan, Frank Schröder, Sebastian Helm, Hans Bleecke

7. New CFD Practices for Modelling High-Speed Flows
Jan Willem van der Burg, Matthias Lühmann, H. Jakob, J. Benton

Part III. Use-Case OPTIMALE

8. Application of Adjoint Based Optimization on a MALE Platform
Kolja Elssel, Kaare Sørensen, Ögmundur Petersson

9. Treating Non-conforming Sensitivity Fields by Mortar Mapping and Vertex Morphing for Multi-disciplinary Shape Optimization
Altuğ Emiroğlu, Roland Wüchner, Kai-Uwe Bletzinger

10. Interfacing MSC Nastran to the CFD-Solver DLR-Tau for Unsteady FSI Analyses with Nonlinear Aircraft Structures
Matthias C. Haupt, Klemens Lindhorst, Peter Horst

Part IV. Use-Case DIMENSyon-P

11. Numerical Computations of Isolated and Installed Engine Jet Flows
Arne Stürmer, Carlos Màrquez-Gutierrez, Peer Böhning

12. Application of Reynolds-Stress-Models on Free Shear Layers
Tim Landa, René-Daniel Cécora, Rolf Radespiel

13. Further Development of CAA Simulation for Isolated and Installed Nozzle Configurations
Andrej Neifeld, Roland Ewert

Part V. Cross-Cutting Subjects

14. Structural Optimization of 3D Wings Under Aerodynamic Loads: Topology and Shell
Volker Schulz, Roland Stoffel, Heinz Zorn

15. Accelerating Unsteady CFD Simulations Using a Minimum Residual Based Nonlinear Reduced Order Modeling Approach
Matteo Ripepi, Stefan Görtz

16. Surrogate-Based Aerodynamic Shape Optimization of a Wing-Body Transport Aircraft Configuration
Zhong-Hua Han, Mohammad Abu-Zurayk, Stefan Görtz, Caslav Ilic

17. A Method for the Calculation of Large Deformations in Aeroelastic Applications
Markus Ritter

Avainsanat: Engineering, Vibration, Dynamical Systems, Control, Aerospace Technology and Astronautics, Numerical and Computational Physics, Simulation, Fluid- and Aerodynamics