Анализ устойчивости вертолета при раскрутке несущего винта на земле

Николаев, Е.И.; Пантюхин, К.Н.

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Full metadata record

DC Field	Value	Language
dc.contributor.author	Николаев, Е.И.
dc.contributor.author	Пантюхин, К.Н.
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:42Z	-
dc.date.available	2025-08-27T05:14:42Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171218\66489
dc.identifier.citation	Николаев, Е. И. Анализ устойчивости вертолета при раскрутке несущего винта на земле = Analysis of stability helicopter by rotor starting on the groundr / Е. И. Николаев, К. Н. Пантюхин // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 292-293.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20479	-
dc.description.abstract	Stable of motion a single rotor helicopter on the ground is investigating. It has six degree of freedom fuselage and flapping motion of blades.
dc.language	rus
dc.publisher	СГАУ
dc.title	Анализ устойчивости вертолета при раскрутке несущего винта на земле
dc.title.alternative	Analysis of stability helicopter by rotor starting on the ground
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Analiz-ustoichivosti-vertoleta-pri-raskrutke-nesushego-vinta-na-zemle-66489
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Analiz-ustoichivosti-vertoleta-pri-raskrutke-nesushego-vinta-na-zemle-66489
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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File	Description	Size	Format
292-293.pdf	Основная статья	1.4 MB	Adobe PDF	View/Open

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