Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/25367
Full metadata record
DC FieldValueLanguage
dc.contributor.authorSineglazov, Viktoren
dc.contributor.authorZiganshin, Anvaren
dc.date.accessioned2017-03-17T07:16:51Z-
dc.date.available2017-03-17T07:16:51Z-
dc.date.issued2015-10-
dc.identifier.isbn978-1-4673-6566-6-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/25367-
dc.descriptionUkraine Section SP/AES Joint Chapteren
dc.description.abstractThe range of geometric parameters describing the airfoil form was determined. The computer aided design method to optimize these geometric parameters on the base of genetic algorithm was created.uk_UA
dc.language.isoenen
dc.publisherOsvita Ukrainyen
dc.relation.ispartofseriesCFP1529V-PRT;Session A 45-47en
dc.relation.ispartofseriesIEEE 3rd International Conference;en
dc.subjectаerodynamicsen
dc.titleComputer Aided Design of Wing with Given Characteristicsen
dc.typeArticleen
dc.specialityAdvanced Methods of Computer-Aided Design, Aerodynamics, Flight-Technical Characteristics, Durability of UAVen
Appears in Collections:Матеріали наукових, науково-практичних конференцій кафедри авіаційних комп'ютерно-інтегрованих комплексів

Files in This Item:
File Description SizeFormat 
45-47.pdfОсновная статья477.5 kBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.