Axial and vertical layout of forewing on canard configuration influence of longitudinal stability

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DC Field	Value	Language
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:44Z	-
dc.date.available	2025-08-27T05:14:44Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171221\66550
dc.identifier.citation	Selezneva, D. A. Axial and vertical layout of forewing on canard configuration influence of longitudinal stability / D. A. Selezneva, Wumaierjiang Muketaer, Ji Simei, V. G. Shakhov // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 349-350.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20489	-
dc.description.abstract	This paper focus on the axial and vertical position of front wing influence the longitudinal stability of canard configuration. Use the 3-D vortex lattice software to simulate and calculate.
dc.language	en
dc.publisher	СГАУ
dc.title	Axial and vertical layout of forewing on canard configuration influence of longitudinal stability
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Axial-and-vertical-layout-of-forewing-on-canard-configuration-influence-of-longitudinal-stability-66550
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Axial-and-vertical-layout-of-forewing-on-canard-configuration-influence-of-longitudinal-stability-66550
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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