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NASA-TR-R-300

Aerodynamic forces on a stationary and oscillating circular cylinder at high Reynolds numbers

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:29:42Z
date available2017-09-04T17:29:42Z
date copyright01/01/1969
date issued1969
identifier otherCSWWAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/152763
description abstractTransonic wind tunnel tests of aerodynamic drag and lift forces on circular cylinder in two dimensional flow at high Reynolds number
languageEnglish
titleNASA-TR-R-300num
titleAerodynamic forces on a stationary and oscillating circular cylinder at high Reynolds numbersen
typestandard
page67
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1969
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsCIRCULAR
subject keywordsCYLINDERS
subject keywordsDIMENSIONAL
subject keywordsDRAG
subject keywordsFLOW
subject keywordsLIFT
subject keywordsLOADS
subject keywordsNUMBER
subject keywordsOSCILLATING
subject keywordsPRESSURE
subject keywordsRANDOM
subject keywordsREYNOLDS
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSTROUHAL
subject keywordsTESTS
subject keywordsTRANSONIC
subject keywordsTUNNEL
subject keywordsTUNNELS
subject keywordsTWO
subject keywordsWIND


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