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Basic turbine cascade flow experiments

Petersen, Anna (2015) Basic turbine cascade flow experiments. DLR-Interner Bericht, Project Report. IB 225 – 2015 A 05, 34 S.

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Official URL: http://tfast.eu/

Abstract

DLR has to submit two deliverables in Workpackage 4. These contain several measurement techniques applied at a straight turbine cascade. The measurements are divided in two parts. This report includes measurements with and without cooling. The second part contains measurements with the former cooling configuration and air jet vortex generators (AJVG ́s), additionally. The second report will be delivered at the end of the project. The profile contour was designed by RRD and handed over at the beginning of the project. Besides do other partners numerical simulations for these flow cases. The following measurement techniques are applied: Schlieren technique, Infrared thermography, Hot-wire anemometry, Pressure tapping’s, Wake traverses. The hot-wire anemometry was deployed to investigate the inflow conditions. These results were already handed over to the partners, who adopt the numerical part, for their inlet boundary conditions. The measurements are utilized to compare them with the numerical results. This report is subdivided in the description of the wind tunnel system, the metrology, a subsequent chapter about uncertainties estimations and the presentation of the measurements will be done in the chapter Results and Discussion.

Item URL in elib:https://elib.dlr.de/100927/
Document Type:Monograph (DLR-Interner Bericht, Project Report)
Additional Information:TFAST Project—Transition Location Effect on Shock Wave Boundary Layer Interaction
Title:Basic turbine cascade flow experiments
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Petersen, Annaanna.petersen (at) dlr.dehttps://orcid.org/0000-0003-4819-4994
Date:December 2015
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:34
Status:Accepted
Keywords:Straight turbine cascade, infrared, hot-film, loss coefficient, Schlieren technique, transition location, film cooling
Institution:Institut für Antriebstechnik
Department:Turbine
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:propulsion systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Turbine Technologies
Location: Göttingen
Institutes and Institutions:Institute of Propulsion Technology > Turbine
Deposited By: Petersen, Anna
Deposited On:02 Jan 2016 16:52
Last Modified:31 Jul 2019 19:58

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