Lift of the nose droop airfoil

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DC Field	Value	Language
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:46Z	-
dc.date.available	2025-08-27T05:14:46Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171225\66649
dc.identifier.citation	Frolov, V. A. Lift of the nose droop airfoil / Vladimir A. Frolov, Yang Hao // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 390-392.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20515	-
dc.description.abstract	A model for the potential circulation flow around nose droop airfoil has been proposed. The solution is obtained for the flow of incompressible ideal fluid. The Complex Variable Function Theory, Method of Discrete Vortices(MDV) and numerical-analytical method (NAM) are applied. Dependence of the lift on the angle of attack, relative length of the nose droop and its angle of deflection is obtained.
dc.language	rus
dc.publisher	СГАУ
dc.title	Lift of the nose droop airfoil
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Lift-of-the-nose-droop-airfoil-66649
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Lift-of-the-nose-droop-airfoil-66649
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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