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The influence of a special fillet between the endwall and airfoil at the leading edge on the performance of the turbine nozzle diaphragm
(Siemens LLC Energy Oil & Gas Design Department)
KTH, School of Industrial Engineering and Management (ITM), Energy Technology, Heat and Power Technology.ORCID iD: 0000-0001-5162-2289
KTH, School of Industrial Engineering and Management (ITM), Energy Technology, Heat and Power Technology.ORCID iD: 0000-0002-1033-9601
2013 (English)In: Thermal Engineering, ISSN 0040-6015, Vol. 60, no 3, 217-222 p.Article in journal (Refereed) Published
Abstract [en]

It is shown from the results of experimental investigations carried out on a nozzle diaphragm’s sector that an enlarged fillet at the vane leading edge does not have an essential effect on the flow and energy losses in the nozzle diaphragm

Place, publisher, year, edition, pages
Maik Nauka/Interperiodica, 2013. Vol. 60, no 3, 217-222 p.
Keyword [en]
nozzle diaphragm, fillet, end losses, flow exit angle and vortex structure
National Category
Energy Engineering Applied Mechanics
Research subject
SRA - Energy
Identifiers
URN: urn:nbn:se:kth:diva-118950DOI: 10.1134/S0040601513020055Scopus ID: 2-s2.0-84879681734OAI: oai:DiVA.org:kth-118950DiVA: diva2:609198
Funder
StandUp
Note

QC 20130603

Available from: 2013-03-04 Created: 2013-03-04 Last updated: 2017-03-30Bibliographically approved

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Saha, RanjanFridh, Jens

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