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NACA-TM-1285

Investigations of the wall-shearing stress in turbulent boundary layers

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:55:40Z
date available2017-09-04T15:55:40Z
date copyright01/01/1950
date issued1950
identifier otherBEYIYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/59002
description abstractBecause of the unsatisfactory state of knowledge concerning the surface shearing stress of boundary layers with pressure gradients, the problem is re-examined. It is found that for general turbulent boundary layers in wall proximity, that is, in the laminar sublayer, in the transition zone and in the part of the completely turbulent zone near the wall, the same universal law applies as for the plate flow.
languageEnglish
titleNACA-TM-1285num
titleInvestigations of the wall-shearing stress in turbulent boundary layersen
typestandard
page26
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1950
contenttypefulltext
subject keywordsBOUNDARY
subject keywordsDISTRIBUTION
subject keywordsEFFECT
subject keywordsFLAT
subject keywordsFLOW
subject keywordsFRICTION
subject keywordsGRADIENT
subject keywordsINDICATORS
subject keywordsINSTRUMENTS
subject keywordsLAYER
subject keywordsPLATES
subject keywordsPRESSURE
subject keywordsSHEARING
subject keywordsSKIN
subject keywordsSTRESS
subject keywordsTURBULENT
subject keywordsVELOCITY
subject keywordsWALLS


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