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The application of a pressure sensitive paint for measurements in a linear cascade

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.

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:
AuthorsInstitution or Email of Authors
de Graaf, F.R.UNSPECIFIED
Date:1994
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: elib DLR-Beauftragter
Deposited On:03 Apr 2006
Last Modified:27 Apr 2009 10:08

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