Show simple item record

Influence of trailing edge tab on moment characteristic of the airfoil NACA 23012

dc.contributor.authorLasauskas, Eduardas
dc.contributor.authorLutz, Th
dc.contributor.authorDietz, M
dc.date.accessioned2023-09-18T19:48:11Z
dc.date.available2023-09-18T19:48:11Z
dc.date.issued2007
dc.identifier.other(BIS)VGT02-000014820
dc.identifier.urihttps://etalpykla.vilniustech.lt/handle/123456789/143482
dc.format.extentp. 26
dc.format.mediumtekstas / txt
dc.language.isoeng
dc.titleInfluence of trailing edge tab on moment characteristic of the airfoil NACA 23012
dc.typeKonferencijos pranešimo santrauka / Conference presentation abstract
dc.type.pubtypeT2 - Konferencijos pranešimo tezės / Conference presentation abstract
dc.contributor.institutionVilniaus Gedimino technikos universitetas
dc.contributor.facultyAntano Gustaičio aviacijos institutas / Antanas Gustaitis Aviation Institute
dc.subject.researchfieldT 009 - Mechanikos inžinerija / Mechanical enginering
dcterms.sourcetitleAviation-2007 & Aviation technologies : abstracts of the international conferences, held on April 18, 2007, Vilnius, Lithuania
dc.publisher.nameTechnika
dc.publisher.cityVilnius
dc.identifier.elaba3783740


Files in this item

FilesSizeFormatView

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record