Workshop on Turbomachinery Aerodynamic and Multidisciplinary Optimization: Current state of the art and future trends
Tuesday 15 November 2016 - Wednesday 16 November 2016VKI Secretariat: This email address is being protected from spambots. You need JavaScript enabled to view it., Phone: +32 2 359 96 04
programme
Tuesday, 15th of November 2016
- 10:00 Arrival / Welcome
Marcus Meyer, Rolls-Royce Deutschland and Tom Verstraete, Queen Mary University London
- 10:15 Deployment of Optimization Tools in Industry and Integration Into the Design Processes
Christoph Starke, Siemens
- 11:00 Multidisciplinary optimization of turbomachinery components using gradient free and gradient based approaches
Tom Verstraete, Queen Mary University London
- 11:45 Holistic Core Engine Design Optimization: Advances and Challenges Compared to Individual Component Design
Peter Flassig, Rolls-Royce Deutschland
- 12:30 Lunch break (90 mins)
- 14:00 Online surrogate-assisted turbomachinery design optimization at Cenaero
Ingrid Lepot, Cenaero
- 14:45 Overview of optimization activities at ABB Turbo Systems
Kwok-Kai So, ABB
- 15:30 Surrogate model assisted approach to turbomachinery optimization using adjoint or multy fidelity process chains
Christian Voss, DLR
- 16:15 Coffee break (30 mins)
- 16:45 Trends in turbomachinery aerodynamic optimization: A software vendor's point of view
MMattia Brenner, FRIENDSHIP SYSTEMS
- 17:30 The Continuous Adjoint Method in Shape Optimization for Computing Exact Sensitivity Derivatives
Kyriakos Giannakoglou, National Technical University of Athens
- 18:15 End of day 1
Wednesday, 16th of November 2016
- 09:00 Optimization in the face of uncertainty
Andy Keane, University of Southampton
- 09:45 Uncertainty Quantification of manufacturing variability and Robust Design Optimization in turbomachinery
Dirk Wunsch, NUMECA
- 10:30 Coffee break (30 mins)
- 11:00 The impact of modern multi-disciplinary design exploration on improving Aircraft System Design
Durrell Rittenberg, CD-Adapco
- 11:45 CAD parametrisation tools with gradients and application to the TU Berlin stator
Jens-Dominik Mueller, Queen Mary University London
- 12:30 Lunch break (90 mins)
- 14:00 Parameter based 3D Optimization of the „TU Berlin TurboLab Stator“ with ANSYS optiSLang
Johannes Einzinger, ANSYS
- 14:45 Robust multi-objective optimization of an aero engine stator blade based on hybrid surrogate models
Kevin Cremanns, Hochschule Niederrhein
- 15:30 Coffee break (30 mins)
- 16:00 Panel Session: Comparison of the TU Berlin Stator Optimization Results
Marcus Meyer and all participants of the TU Berlin Stator Optimization
- 18:00 End of day 2
Location : von Karman Institute for Fluid Dynamics, Waterloosesteenweg 72, B-1640 Sint-Genesius-Rode