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contributor authorR. W. Miller
contributor authorL. S. Han
date accessioned2017-05-09T01:36:37Z
date available2017-05-09T01:36:37Z
date copyrightJune, 1973
date issued1973
identifier issn0098-2202
identifier otherJFEGA4-26845#237_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163915
description abstractAn approximate integral method of analysis is developed for unsteady laminar boundary layer flows. The case of a flat plate in a free stream with small harmonic velocity oscillations about a steady mean is used to formulate the method. Results are compared with the available experimental data. The essence of the method is to: First obtain asymptotic solutions for limiting cases of the flow under consideration. Then, assume velocity profiles with sufficient generality to include the asymptotic solutions. The profile form functions are determined by applying integral relations (velocity weighted averages of the momentum equation) and compatibility conditions (normal derivatives of the momentum equation evaluated at the boundary). As an example of the method, the second-order mean flow correction is determined for oscillating flow over a flat plate.
publisherThe American Society of Mechanical Engineers (ASME)
titleAnalysis of Unsteady Laminar Boundary Layer Flow by an Integral Method
typeJournal Paper
journal volume95
journal issue2
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3447001
journal fristpage237
journal lastpage247
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsBoundary layers
keywordsEquations
keywordsFlat plates
keywordsMomentum
keywordsOscillations AND Functions
treeJournal of Fluids Engineering:;1973:;volume( 095 ):;issue: 002
contenttypeFulltext


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