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dc.contributor.authorŠnirpūnas, Vincas
dc.date.accessioned2023-09-18T18:55:22Z
dc.date.available2023-09-18T18:55:22Z
dc.date.issued2003
dc.identifier.issn1648-7788
dc.identifier.other(BIS)VGT02-000005600
dc.identifier.urihttps://etalpykla.vilniustech.lt/handle/123456789/133462
dc.description.abstractThis research presents a comparison between the calculated data and the data obtained from the experiment, analyses forced boundary layer’s transition from laminar regime to the turbulent. Attention was paid to airfoil characteristics changes, advantages and disadvantages were analysed. The chosen airfoil is FX63-137. The calculated data were obtained by using the interactive program developed for the design and analysis of subsonic airfoils XFoil6.9. The calculations were compared with laboratory tests results from Notre Dame University in United States of America and from Stuttgart University in Germany. The differences between data were discussed and conclusions were made.eng
dc.format.extentp. 40-44
dc.format.mediumtekstas / txt
dc.language.isoeng
dc.relation.isreferencedbyAcademic Search Complete
dc.relation.isreferencedbyCentral & Eastern European Academic Source (CEEAS)
dc.titleForced boundary layer transition effect on the performance of FX63-137 airfoil at low reynolds numbers
dc.title.alternativeProfilio FX 63-137 charakteristikų tyrimas esant priverstiniam pasienio sluoksnio perėjimui bei mažiems Reinoldso skaičiams
dc.typeStraipsnis kitame recenzuotame leidinyje / Article in other peer-reviewed source
dcterms.references0
dc.type.pubtypeS4 - Straipsnis kitame recenzuotame leidinyje / Article in other peer-reviewed publication
dc.contributor.institutionVilniaus Gedimino technikos universitetas
dc.contributor.facultyAntano Gustaičio aviacijos institutas / Antanas Gustaitis Aviation Institute
dc.subject.researchfieldT 003 - Transporto inžinerija / Transport engineering
dcterms.sourcetitleAviation : research Journal of Vilnius Gediminas Technical University : proceedings of the Fifth International Seminar on ''Recent Researh and Design Progress in Aeronautical Engineering and its Influence on Education'', held on November 27-29, 2002 Vilnius - Lithuania. Part I
dc.description.issueno. 1
dc.description.volumeVol. VII
dc.publisher.nameTechnika
dc.publisher.cityVilnius
dc.identifier.elaba3628365


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