Research output per year
Research output per year
Project Details
Description
The institute operates a transonic test turbine rig for the investigation and development of transonic turbine stages. The test rig allows a pressure ratio of 5, a maximum mass flow of 22 kg/s and a maximum turbine power of 3 MW, so that first and second turbine stages can be tested in full flow similarity. Conventional and optical measurement methods like LDA and PIV are applied to investigate the flow. The measurement of unsteady flow data will help in the understanding of the complex unsteady phenomena in transonic stages and thus help in the future development of more efficient turbines.
| Status | Active |
|---|---|
| Effective start/end date | 1/01/98 → … |
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Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.
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Blade row interaction in a one and a half stage transonic turbine focusing on three dimensional effects - part 1: stator-rotor interaction
Paradiso, B., Persico, B., Gaetani, P., Schennach, O., Pecnik, R. & Woisetschläger, J., 2008, (Accepted/In press) ASME Turbo Expo. .Research output: Chapter in Book/Report/Conference proceeding › Conference paper › peer-review
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Blade row interaction in a one and a half stage transonic turbine focusing on three dimensional effects - part 2: clocking effects
Schennach, O., Paradiso, B., Persico, B., Gaetani, P. & Woisetschläger, J., 2008, (Accepted/In press) ASME Turbo Expo. .Research output: Chapter in Book/Report/Conference proceeding › Conference paper › peer-review
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Experimental and Numerical Flow Visualization in a Transonic Turbine
Woisetschläger, J., Pecnik, R., Göttlich, E., Schennach, O., Marn, A., Sanz, W. & Heitmeir, F., 2008, In: Journal of Visualization. Vol. 11, No. 1, p. 95-102Research output: Contribution to journal › Article › peer-review