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Autorinnen/Autoren:
Bitter, Martin; Kožulović, Dragan
Dokumenttyp:
Zeitschriftenartikel / Journal Article
Titel:
Total pressure losses from planar Particle Image Velocimetry data: A practical approach for accurate wake flow assessment at turbomachinery-relevant Mach & Reynolds numbers
Zeitschrift:
Journal of the Global Power and Propulsion Society
Jahrgang:
9
Veranstalter (Körperschaft):
Global Power & Propulsion Society
Konferenztitel:
Global Power and Propulsion Technical Conference (2024, Chania)
Tagungsort:
Chania, Griechenland
Jahr der Konferenz:
2024
Datum Beginn der Konferenz:
04.09.2024
Datum Ende der Konferenz:
06.09.2024
Jahr:
2024
Seitenbereich:
1-12
Sprache:
Englisch
Abstract:
This work presents a hybrid approach for determining total pressure fields, which were reconstructed from Particle Image Velocimetry data and whose accuracy was raised through in-situ correction with probe-based reference data. The quality of this general approach is validated for turbomachinery-relevant Mach and Reynolds numbers using a cylinder in crossflow as a test case. Furthermore, the approach is applied to investigate the total pressure losses in the wake of a low-pressure turbine cascade. It is shown that the hybrid approach delivers total pressure loss fields over a wide Reynolds and Mach number range, which deviate from the highly accurate integral loss coefficients of a conventional loss traverse with probe-based measurement techniques for compressible flows by an absolute maximum of less than 2 %, but which delivers results at a much higher level of spatial resolution. For incompressible flows, the deviations are almost negligible at < 1%. The paper presents and discusses the exact methodology for both, the collection of experimental data and the outline of the developed approach.
ISSN:
2504-4400
DOI:
10.33737/jgpps/205784
URL zum Inhalt:
https://doi.org/10.33737/jgpps/205784
Institut:
LRT 12 - Institut für Strahlantriebe
Professorin/Professor:
Kožulović, Dragan
Open Access:
Ja / Yes
Open-Access-Lizenz:
CC BY 4.0
URL zur Lizenz:
https://creativecommons.org/licenses/by/4.0/legalcode
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