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de Graaf, F.R. (1994) The application of a pressure sensitive paint for measurements in a linear cascade. DLR-Interner Bericht. 223 - 94 A 19. 57 S.
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Abstract
Pressure measurements on a transonic turbine rotor blade are performed making use of a new technique, a pressure sensitive paint method. The results were compared with the already known pressure distribution, measured by pressure tappings. Recommendations have been made for future measurements.
| Item URL in elib: | https://elib.dlr.de/37166/ | ||||||||
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| Document Type: | Monograph (DLR-Interner Bericht) | ||||||||
| Additional Information: | LIDO-Berichtsjahr=1994, | ||||||||
| Title: | The application of a pressure sensitive paint for measurements in a linear cascade | ||||||||
| Authors: |
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| Date: | 1994 | ||||||||
| Open Access: | No | ||||||||
| Gold Open Access: | No | ||||||||
| In SCOPUS: | No | ||||||||
| In ISI Web of Science: | No | ||||||||
| Number of Pages: | 57 | ||||||||
| Status: | Published | ||||||||
| Keywords: | Pressure sensitive paint, Optical method, Cascade flow, Transonic turbine blade, Pressure distribution | ||||||||
| HGF - Research field: | UNSPECIFIED | ||||||||
| HGF - Program: | Aeronautics | ||||||||
| HGF - Program Themes: | other | ||||||||
| DLR - Research area: | UNSPECIFIED | ||||||||
| DLR - Program: | L TT - Triebwerkstechnologien | ||||||||
| DLR - Research theme (Project): | UNSPECIFIED | ||||||||
| Location: | Köln-Porz , Braunschweig , Göttingen | ||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Institut für Strömungsmechanik > Institut für Experimentelle Strömungsmechanik | ||||||||
| Deposited By: | DLR-Beauftragter, elib | ||||||||
| Deposited On: | 03 Apr 2006 | ||||||||
| Last Modified: | 27 Apr 2009 10:08 |
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