К поиску оптимальной компоновки летательного аппарата с замкнутым крылом

Лазарев, А.Ю.; Семенов, В.Н.

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Full metadata record

DC Field	Value	Language
dc.contributor.author	Лазарев, А.Ю.
dc.contributor.author	Семенов, В.Н.
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:47Z	-
dc.date.available	2025-08-27T05:14:47Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171208\66314
dc.identifier.citation	Лазарев, А. Ю. К поиску оптимальной компоновки летательного аппарата с замкнутым крылом = Searching for optimal configuration of aircraft with annular wings / А. Ю. Лазарев, В. Н. Семенов // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 253-254.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20388	-
dc.description.abstract	A variety of aerodynamic theories do not allows to organize the spatial synthesis of the optimal shape of the aircraft on a unified basis. The procedure for the synthesis of shape based on the FEM model, which is conjugate with the optimization and synthesis of constructive structure. The use of closed circuit and the curvilinear axis of the wing, allow to provide new opportunities to adapt the shape of wing, foils and aircraft to the flight regime
dc.language	rus
dc.publisher	СГАУ
dc.title	К поиску оптимальной компоновки летательного аппарата с замкнутым крылом
dc.title.alternative	Searching for optimal configuration of aircraft with annular wings
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/K-poisku-optimalnoi-komponovki-letatelnogo-apparata-s-zamknutym-krylom-66314
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/K-poisku-optimalnoi-komponovki-letatelnogo-apparata-s-zamknutym-krylom-66314
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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253-254.pdf	Основная статья	1.73 MB	Adobe PDF	View/Open

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