Activities Gas Dynamic Test Facilities
Basic research
- Laminar-turbulent boundary layer transition
- Shock-boundary layer interaction at supersonic inlets
- Modal analysis of fluctuations in boundary layers and in free flow
Measurement techniques
- Further development of hot-wire anemometers
- Development of transient heat flow sensors
- Short-time measurement technology
- Optical methods
Contact

Uwe Gaisbauer
Dr.-Ing.Head of working group Experimental Gas Dynamics