Calculation of laminar boundary layer by integral method for two-fluids upon flat plate

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DC Field	Value	Language
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:28Z	-
dc.date.available	2025-08-27T05:14:28Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171227\66676
dc.identifier.citation	Shakhov, V. G. Calculation of laminar boundary layer by integral method for two-fluids upon flat plate / V. G. Shakhov, Wang Binbin, Ji Simei // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 428-430.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20535	-
dc.description.abstract	In this paper, calculation is done by momentum integral method and based on two-fluids boundary layer. The integral method is an approximate method which can reduce the mathematical difficulties in solving the Navier-Stokes equations in two dimensions. The calculation will be done in MathCAD and Matlab, with the results we figure out that the two-fluids boundary layer has smaller drag than that in general case.
dc.language	en
dc.publisher	СГАУ
dc.title	Calculation of laminar boundary layer by integral method for two-fluids upon flat plate
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Calculation-of-laminar-boundary-layer-by-integral-method-for-twofluids-upon-flat-plate-66676
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Calculation-of-laminar-boundary-layer-by-integral-method-for-twofluids-upon-flat-plate-66676
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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