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NASA-TN-D-5392

Experimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 degrees to 15 degrees

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:25:27Z
date available2017-09-04T18:25:27Z
date copyright01/01/1969
date issued1969
identifier otherIIYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/207651
description abstractPressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 degrees
languageEnglish
titleNASA-TN-D-5392num
titleExperimental pressure distributions for a family of blunt bodies at Mach numbers from 2.49 to 4.63 and angles of attack from 0 degrees to 15 degreesen
typestandard
page88
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1969
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsATTACK
subject keywordsBALLISTICS
subject keywordsBLUNT
subject keywordsBODIES
subject keywordsCYLINDRICAL
subject keywordsDATA
subject keywordsDISTRIBUTION
subject keywordsHEATING
subject keywordsMODELS
subject keywordsPRESSURE
subject keywordsREENTRY
subject keywordsREVOLUTION
subject keywordsSPEED
subject keywordsSUPERSONIC
subject keywordsTABLES
subject keywordsTUNNEL
subject keywordsVEHICLES
subject keywordsWIND


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