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Equipment of Institute of Fluid Mechanics

Institute of Fluid Mechanics
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Control valve for steam turbines

Facility: Chair for Turbomachinery and Flight Propulsion

Scaled control valve for the experimental investigation of the valve's unsteady operating behaviour.

 

High resolution photogrammetry camera

Manufacturer: GOM GmbH
Model: ATOS Plus
Facility: Chair for Turbomachinery and Flight Propulsion

"The photogrammetry camera delivers up to 29 megapixel resolution capturing high accuracy reference points." [www.gom.com]

 

High resolution, optical 3d-digitizer

Manufacturer: GOM GmbH
Model: ATOS Triple Scan
Facility: Chair for Turbomachinery and Flight Propulsion

"ATOS Triple Scan is a high resolution, optical digitizer that delivers rapid and precise three-dimensional measuring data for the optimization of design processes..." [www.gom.com]

 

ATOS ScanBox

Manufacturer: GOM GmbH
Model: 5108
Facility: Chair for Turbomachinery and Flight Propulsion

ATOS ScanBox - A comprehensive system for automated scan using fringe projection.

 

Deflector Wind Tunnel (UGWK)

Facility: Chair for Turbomachinery and Flight Propulsion

Deflector Wind Tunnel is a continuously operating open wind tunnel in suction mode (Eiffel channel).

 

Plate film cooling channel (PFKK)

Facility: Chair for Turbomachinery and Flight Propulsion

Plate film cooling channel - A rectangular channel for the investigation of film cooling, and internal heat transfer in the cooled turbine blades.

 

Transonic Turbines Cascade Wind Tunnel (TTGWK)

Facility: Chair for Turbomachinery and Flight Propulsion

Transonic Turbines Cascade Wind Tunnel for the investigation of transonic turbine cascades at very low aspect ratios.

 

Low Speed Research Compressor (LSRC)

Facility: Chair for Turbomachinery and Flight Propulsion

The Low Speed Research Compressor is a scaled, low-speed 1- to 4-stage compressor model. It is used for the investigation of flow structures at the stability limit of compressors.

 

Cascade Wind Tunnel (GWK)

Facility: Chair for Turbomachinery and Flight Propulsion

The Cascade Wind Tunnel is a continuously operating, open wind tunnel. It's used for the investigation of turbine or compressor bladings.

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