Please use this identifier to cite or link to this item:
https://hdl.handle.net/20.500.11851/9883
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Topal, A. | - |
dc.contributor.author | Çatori, C. | - |
dc.contributor.author | Çağan, L. | - |
dc.contributor.author | Uslu, S. | - |
dc.contributor.author | Turan, Ö. | - |
dc.contributor.author | Pişkin, A. | - |
dc.date.accessioned | 2022-12-25T20:51:50Z | - |
dc.date.available | 2022-12-25T20:51:50Z | - |
dc.date.issued | 2014 | - |
dc.identifier.isbn | 9.78E+12 | - |
dc.identifier.issn | 2578-5486 | - |
dc.identifier.uri | https://doi.org/10.1615/ICHMT.2014.IntSympConvHeatMassTransf.230 | - |
dc.identifier.uri | https://hdl.handle.net/20.500.11851/9883 | - |
dc.description | International Symposium on Convective Heat and Mass Transfer, CONV 2014 -- 8 June 2014 through 13 June 2014 -- 268949 | en_US |
dc.description.abstract | A gas turbine combustor preliminary design tool that includes all the conceptual and one-dimensional preliminary design process in an automated way has been used for the heat transfer calculations. The flame tube wall temperature characteristics of an experimental through flow combustor with air-blast atomizer has been analysed using the methodology. A small scale gas turbine combustor is used as a test case in order to validate the predictive capability of the newly developed methodology named PreCoDe. Predictions about the mass flow split, flame and combustor liner temperatures for 1 millimetre segments have been performed by using the PreCoDe technique that makes use of analytical and empirical correlations. For the validation of the code, calculation results are compared with the thermal paint and the thermocouple temperature measurements on the combustor liner. As a conclusion, the 1D prediction has revealed good agreement with experimental results and hence good design capability and potentials of the PreCoDe. © 2014, Begell House Inc. All rights reserved. | en_US |
dc.description.sponsorship | ACKNOWLEDGEMENTS The authors would like to thank colleagues at TEI, Tusas Engine Industries for the contribution of the experimental studies. Numerical studies installation of the atmospheric combustor test rig and conducted experimental studies were a part of the “Development of a Combustion Chamber with Air-blast Fuel-Air Injector” project (00564.STZ.2010-1) and financially supported by the Turkish Republic Ministry of Science, Industry and Technology. The authors would like to thank to the ministry for the invaluable support. | en_US |
dc.language.iso | en | en_US |
dc.publisher | Begell House Inc. | en_US |
dc.relation.ispartof | International Symposium on Advances in Computational Heat Transfer | en_US |
dc.rights | info:eu-repo/semantics/closedAccess | en_US |
dc.title | One-dimensional heat transfer analysis and experimental investigation of a gas turbine combustor | en_US |
dc.type | Conference Object | en_US |
dc.department | ESTÜ | en_US |
dc.identifier.startpage | 319 | en_US |
dc.identifier.endpage | 333 | en_US |
dc.identifier.scopus | 2-s2.0-85057135184 | en_US |
dc.institutionauthor | [Belirlenecek] | - |
dc.identifier.doi | 10.1615/ICHMT.2014.IntSympConvHeatMassTransf.230 | - |
dc.authorscopusid | 56432596100 | - |
dc.authorscopusid | 56433573000 | - |
dc.authorscopusid | 56433128600 | - |
dc.authorscopusid | 56432570700 | - |
dc.authorscopusid | 54394470800 | - |
dc.authorscopusid | 56439598000 | - |
dc.relation.publicationcategory | Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı | en_US |
dc.identifier.trdizinid | en_US] | |
item.cerifentitytype | Publications | - |
item.openairecristype | http://purl.org/coar/resource_type/c_18cf | - |
item.grantfulltext | none | - |
item.fulltext | No Fulltext | - |
item.languageiso639-1 | en | - |
item.openairetype | Conference Object | - |
Appears in Collections: | Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection |
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