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Experimental pressure distributions on a 120 degrees cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0 degrees to 20 degrees

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:50:45Z
date available2017-09-04T15:50:45Z
date copyright01/01/1969
date issued1969
identifier otherQHYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/53871
description abstractExperimental pressure distributions on 120 deg cone at Mach 2.96 to 4.63 and angles of attack from 0 deg to 20 deg
languageEnglish
titleNASA-TN-D-5054num
titleExperimental pressure distributions on a 120 degrees cone at Mach numbers from 2.96 to 4.63 and angles of attack from 0 degrees to 20 degreesen
typestandard
page79
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1969
contenttypefulltext
subject keywordsBLUNT
subject keywordsBODIES
subject keywordsCONES
subject keywordsDISTRIBUTION
subject keywordsFLOW
subject keywordsFRUSTUMS
subject keywordsMACH
subject keywordsNUMBER
subject keywordsPRESSURE
subject keywordsPROFILES
subject keywordsSHOCK
subject keywordsSLENDER
subject keywordsSUPERSONIC
subject keywordsWAVE


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