Activities Gas Dynamic Test Facilities
Supersonic channels in the so-called "suck-down" principle
- Mach number range 1,5 - 3,0
- Measurement times up to 3 minutes
- Medium supersonic wind tunnel designed as a so-called half-model channel
- Measurement technology used: hot-wire hot-film anemometry, pressure and temperature sensors, heat flow sensors and optical methods
Projekts and research
Research Topics:
- Laminar-turbulent boundary layer transition
- Shock-boundary layer interaction at supersonic inlets and optical methods
- Spurious mode detection in boundary layers and free flow
- Development of a new hypersonic wind channel
Contact

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