Laminar Wind Tunnel

Institute of Aerodynamics and Gas Dynamics

Based on a sound record in the development and testing of natural laminar flow (NLF) airfoil section, the focus of the working group is put on the impact of unsteady inflow conditions on laminar boundary layer stability and transition. This includes the development of novel measurement procedures as well as improvements of transition prediction tools.

The airfoils developed in the last 40 years are used world wide in gliders, small and medium motor aircrafts, helicopters, wind-farms, propellers etc.

For our measurements the following Wind Tunnels are available

Laminar Wind Tunnel

The Laminar Wind Tunnel

The Model Wind Tunnel

The Model Wind Tunnel

  • more about the Model Wind Tunnel
    The Model Wind Tunnel was constructed especially for model gliders profiles and is mainly used for student's theses and activities.
The Gust Wind Tunnel

The Gust Wind Tunnel

[Photos: iag uni stuttgart, iag uni stuttgart, iag uni stuttgart]

Technology Transfer

Within the framework of technology transfer we carry out measurements for industry partners and also act in an advisory capacity to domestic and foreign aircraft designers.
 

                                                    

(Icon: pdf)

Call for applications Student thesis with the topic: Kennfeldermittllung elektrischer Luftfahrtantriebe

Team Laminar Wind Tunnel

All members of the working group Laminar Wind Tunnel

Research and Projects

of the workgroup Laminar Wind Tunnel

Publications

of the Laminar Wind Tunnel Workgroup

Teaching Laminar Wind Tunnel

Lectures of Dr.-Ing Werner Würz

Contact

This image shows Ulrich Deck, M.Sc.

Ulrich Deck, M.Sc.

 

Head of working group Laminar Wind Tunnel

To the top of the page