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contributor authorH. E. Weber
date accessioned2017-05-08T23:05:06Z
date available2017-05-08T23:05:06Z
date copyrightJune, 1978
date issued1978
identifier issn0098-2202
identifier otherJFEGA4-26933#232_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/91197
description abstractA simple, semiempirical method for calculating the laminar, transition, and turbulent boundary layer with arbitrary free stream pressure gradient is developed. Good correlation is obtained with data on general two dimensional turbulent flows, diffuser flows, and the cylinder in cross-flow. However only for the diffuser has the boundary layer flow been coupled with the potential core so that only the inlet conditions and geometry are required. In other cases the free stream velocity distribution must be known or calculable. Skin friction coefficient, momentum thickness Reynolds number, and free stream pressure gradient parameter correlation employs a simple lag theory. With the integral momentum equation the complete boundary layer parameters are obtained as functions of the distance along a surface.
publisherThe American Society of Mechanical Engineers (ASME)
titleBoundary Layer Calculation for Analysis and Design
typeJournal Paper
journal volume100
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3448637
journal fristpage232
journal lastpage236
identifier eissn1528-901X
keywordsBoundary layers
keywordsDesign
keywordsMomentum
keywordsFlow (Dynamics)
keywordsPressure gradient
keywordsDiffusers
keywordsThickness
keywordsCross-flow
keywordsTurbulence
keywordsReynolds number
keywordsSkin friction (Fluid dynamics)
keywordsBoundary layer turbulence
keywordsCylinders
keywordsEquations
keywordsFunctions AND Geometry
treeJournal of Fluids Engineering:;1978:;volume( 100 ):;issue: 002
contenttypeFulltext


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