Подъёмная сила аэродинамического профиля с интерцептором

Редькина, К.В.; Фролов, В.А.

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Full metadata record

DC Field	Value	Language
dc.contributor.author	Редькина, К.В.
dc.contributor.author	Фролов, В.А.
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:31Z	-
dc.date.available	2025-08-27T05:14:31Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171220\66539
dc.identifier.citation	Редькина, К. В. Подъёмная сила аэродинамического профиля с интерцептором = Lift of the airfoil with spoiler / К. В. Редькина, В. А. Фролов // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 333-334.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20411	-
dc.description.abstract	A model of a stationary vortex for the potential circulation flow around airfoil-spoiler combination has been proposed. The solution is obtained for the flow of incompressible ideal fluid. The Complex Variable Function Theory is applied. For the simulation of the recirculation area, a stationary vortex is used, the location of which is found by minimizing a velocity function. Dependence of the lift on the angle of attack, relative length of the spoiler and its angle of deflection is obtained.
dc.language	rus
dc.publisher	СГАУ
dc.title	Подъёмная сила аэродинамического профиля с интерцептором
dc.title.alternative	Lift of the airfoil with spoiler
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Podemnaya-sila-aerodinamicheskogo-profilya-s-interceptorom-66539
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Podemnaya-sila-aerodinamicheskogo-profilya-s-interceptorom-66539
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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File	Description	Size	Format
333-334.pdf	Основная статья	1.71 MB	Adobe PDF	View/Open

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