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NASA-TM-78813

Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from minus 4 deg to 60 deg

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:48:56Z
date available2017-09-04T15:48:56Z
date copyright01/01/1979
date issued1979
identifier otherQCNKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/51865
description abstractFlow visualization and force data for a series of six bodies of revolution are presented without analysis. The data were obtained in the Langley Unitary Plan wind tunnel for angles of attack from -4 deg to 60 deg. The Reynolds number used for these tests was 6,600,000 per meter.
languageEnglish
titleNASA-TM-78813num
titleWind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from minus 4 deg to 60 degen
typestandard
page268
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1979
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsATTACK
subject keywordsBODIES
subject keywordsCONFIGURATIONS
subject keywordsDATA
subject keywordsFLOW
subject keywordsFORCES
subject keywordsMACH
subject keywordsMISSILE
subject keywordsNUMBER
subject keywordsREVOLUTION
subject keywordsTABLES
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsVISUALIZATION
subject keywordsWIND


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