Towards Effective Flow Control
and Mitigation of Shock Effects
In Aeronautical Applications
Towards Effective Flow Control
and Mitigation of Shock Effects
In Aeronautical Applications
This project has recieved funding from the European Union’s Horizon 2020 research and innovation programme under grant agreement No EC grant 860909. This project has recieved funding from
the European Union’s Horizon 2020 research and innovation programme
under grant agreement No EC grant 860909.About
The aviation industry is entering an era of new technologies and requires high-performance wings, control surfaces, intakes and turbo machinery blades, where transgenic flow is common and the formation of shock waves is the key aerodynamic challenge.
The main objective of TEAMAero is to develop new scientific knowledge, capabilities and technologies for the aeronautics industry. The researchers recruited in TEAMAero will investigate emerging technologies through laboratory experiments, theoretical modeling and numerical simulations addressing aspects of shock wave boundary layer interaction (SBLI) and flow control methods.
1
to improve our fundamental understanding of the physics of Shock Wave Boundary Layer Interaction, including three-dimensionality and unsteadiness
2
to identify the flow domains best suited to flow-control device installation
3
to develop flow-control schemes using wall transpiration (suction/blowing), vortex generators and surface treatments to delay the onset of separation
4
to develop novel numerical methods for predicting the effects of Shock Wave Boundary Layer Interaction