Sie befinden Sich nicht im Netzwerk der Universität Paderborn. Der Zugriff auf elektronische Ressourcen ist gegebenenfalls nur via VPN oder Shibboleth (DFN-AAI) möglich. mehr Informationen...
International Journal of Gas Turbine, Propulsion and Power Systems, 2024, Vol.15(1), pp.1-8
2024
Volltextzugriff (PDF)

Details

Autor(en) / Beteiligte
Titel
Effect of Crossflow-to-Jet Temperature Ratio on Heat Transfer and Flow of Impingement Cooling
Ist Teil von
  • International Journal of Gas Turbine, Propulsion and Power Systems, 2024, Vol.15(1), pp.1-8
Ort / Verlag
Gas Turbine Society of Japan
Erscheinungsjahr
2024
Quelle
EZB Electronic Journals Library
Beschreibungen/Notizen
  • This paper studied an array impingement cooling with different temperature initial crossflow. Both the heat transfer and flow field of impingement cooling with four crossflow-to-jet temperature ratios (TR=1.0, 1.1, 1.2, 1.3) under four crossflow-to-jet mass flow ratios (CMFR=0.3, 0.5, 0.7, 0.9) and four jet Reynolds numbers (Rej=15,000, 25,000, 35,000, 45,000) are investigated. Results show that (1) as the Rej increases, the Nusselt number increases, but the friction loss coefficient decreases; (2) as the CMFR increases, Nusselt number and friction loss coefficient decrease; (3) as the TR increases, the Nusselt number always decreases, but the variation of friction loss coefficient is related to CMFR. To be specific, when the CMFR are 0.3 and 0.5, the friction loss coefficient decreases with the increase of TR, but when the CMFR are 0.7 and 0.9, it increases as the TR increases. The research results will clarify the effect mechanism of TR on impingement cooling.
Sprache
Englisch
Identifikatoren
ISSN: 1882-5079
eISSN: 1882-5079
DOI: 10.38036/jgpp.15.1_1
Titel-ID: cdi_jstage_primary_article_jgpp_15_1_15_vol15no1tp01_article_char_en
Format

Weiterführende Literatur

Empfehlungen zum selben Thema automatisch vorgeschlagen von bX