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

Title:	Axial and vertical layout of forewing on canard configuration influence of longitudinal stability
Issue Date:	2012
Publisher:	СГАУ
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.
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.
URI:	http://repo.ssau.ru/jspui/handle/123456789/20489
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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File	Description	Size	Format
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