The workshop is organised as a part of dissemination activities of the MSCA-ITN-ETN TEAMAero project (https://h2020-teamaero.eu/)
and the main objective is a shock wave boundary layer interaction (SBLI) and flow control.

The main topic of the workshop is shock wave boundary layer interaction (SBLI) and flow control, with a focus on:

- unsteadiness and transitional mechanism of SBLI,
- boundary layer and surface roughness effect on SBLI,
- shock induced fluid-structure interactions,
- transition and buffet control with flow control devices,
- numerical and experimental tripping of high-speed turbulent boundary layer,
- from high-fidelity high-order to reduced-order modelling for unsteady SBLI.

Invited speakers:

• Markus Fischer (DLR) - topic: Flow Control for Civil Aircrafts
• Frank Haselbach (Airbus) - topic: Engine Design and Integration - Today and Tomorrow

During the workshop results of the MSCA-ITN-ETN TEAMAero project (https://h2020-teamaero.eu/) will be presented:

1. Numerical investigations of SBLI and flow control on compressor blades including transition effects (Rolls-Royce Deutschland)
2. Effects of Shock Boundary Layer Interaction with High Loading And Strong Adverse Pressure Gradients (Rolls-Royce Deutschland)
3. Experimental and numerical investigation of flow control on a transonic compressor cascade (DLR - Institute of Propulsion)
4. Transitional and turbulent flow conditions in a shock/boundary layer interaction: an experimental study (Universite d’aix Marseille)
5. Numerical study (LES) of a separated SBLI with altered reattachment (Universite d’aix Marseille)
6. Characterization of shock wave/boundary layer interaction control by perforated plates (ONERA)
7. Investigation of unsteady three-dimensional shock/boundary-layer interactions and flow control to mitigate corner separation (University of Cambridge)
8. Investigation and control of supersonic shock boundary layer interactions and shock induced fluid-structure interactions (Technische Universiteit Delft)
9. Stability study of unsteady separated flows(University of Glasgow)
10. From high-fidelity high-order to reduce-order modelling for unsteady shock wave boundary layer interactions (Cadence Design Systems)
11. Development of numerical tools for high-fidelity simulation of shock/boundary layer interactions (Universita Degli Studi di Roma La Sapienza)
12. Numerical investigation of transition and buffet control with flow control devices (Institut National Polytechnique de Toulouse)
13. Experimental investigations on transitional Shock-BL-Interaction with flow control devices (Technische Universitat Berlin)
14. Investigation of shock wave effects in highly loaded compressor stator (IMPPAN)
15. Shock wave boundary layer interaction on compressor rotor profile with flow control (IMPPAN)

Registration:

On-site participation: Free
On-line participation: Free
Conference Dinner (Day-1): 60 EUR