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NACA-TR-1036

Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a Mach number 1.5

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:44:07Z
date available2017-09-04T16:44:07Z
date copyright01/01/1951
date issued1951
identifier otherVWDZYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/107419
description abstractModels were tested to evaluate effects of Reynolds number for both laminar and turbulent boundary layers. Principal geometric variables investigated were afterbody shape and length-diameter ratio. Force tests and base-pressure measurements were made. Schlieren photographs were used to analyze the effects of viscosity on flow separation and shock-wave configuration and to verify the condition of the boundary layer as deduced from the force tests. The results are discussed and compared with theoretical calculations.
languageEnglish
titleNACA-TR-1036num
titleExperimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a Mach number 1.5en
typestandard
page24
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1951
contenttypefulltext
subject keywordsAFTERBODIES
subject keywordsBASE
subject keywordsBODIES
subject keywordsBOUNDARY
subject keywordsCOMPARISON
subject keywordsCONFIGURATIONS
subject keywordsDRAG
subject keywordsFLOW
subject keywordsFRICTION
subject keywordsINDEPENDENT
subject keywordsLAMINAR
subject keywordsLAYER
subject keywordsMACH
subject keywordsNUMBER
subject keywordsPRESSURE
subject keywordsREVOLUTION
subject keywordsREYNOLDS
subject keywordsROUGHNESS
subject keywordsSEPARATION
subject keywordsSHOCK
subject keywordsSKIN
subject keywordsSPEED
subject keywordsSUPERSONIC
subject keywordsSURFACE
subject keywordsTESTS
subject keywordsTHEORIES
subject keywordsTRANSITION
subject keywordsTUNNEL
subject keywordsTURBULENT
subject keywordsVARIABLES
subject keywordsVISCOUS
subject keywordsWAVES
subject keywordsWIND


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