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dc.contributor.authorWenhang, Luo
dc.date.accessioned2023-07-07T09:48:22Z
dc.date.available2023-07-07T09:48:22Z
dc.date.issued2023
dc.identifier.citationWenhang, L. Design of composite wing structure of the light aircraft : explanatory note to the master's thesis project : 134 – aerospace engineering / L. Wenhang ; Nat. Aerospace Univ. nam. M. Ye. Zhukovsky «Kharkiv Aviation Inst.», Fac. of aircraft engineering, Airplane and helicopter des. dep. (№ 103) ; supervisor O. Soboliev. – Kharkiv, 2023. – 104 p.uk_UA
dc.identifier.urihttp://dspace.library.khai.edu/xmlui/handle/123456789/5205
dc.description.abstractThe purpose of the work: Develop technical requirements specification, research statistical data analy sis of scientists, who dealt with vehicle and what issues they claim and give the rationale for the choice of the scientific research of light aircraft area, b y referring to factual data from the prototype, citing its advantages and strengths, it is clear that the advantages of the design of this project's light aircraft, based on theoretical experience, lie in its long range, compact size, good stability, and the proposal of a plan to increase the strength of the wing structure by using composite material layers.uk_UA
dc.description.abstractМета роботи: розробити технічні вимоги, статистичні дані досліджень науковців, які займалися автотранспортом і які проблеми вони висувають та обґрунтувати вибір напряму наукового дослідження легкої авіації, посилаючись на фактичні дані з прототипу.uk_UA
dc.language.isoenuk_UA
dc.subjectlightaircraftuk_UA
dc.subjectcomposit materialuk_UA
dc.subject3D modelinguk_UA
dc.subjectcarbonuk_UA
dc.subjectлегка авіаціяuk_UA
dc.subjectкомпозитний матеріалuk_UA
dc.subject3D моделюванняuk_UA
dc.subjectкарбонuk_UA
dc.titleDesign of composite wing structure of the light aircraftuk_UA
dc.typeMastersWorkuk_UA


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