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NASA-TN-D-2042

Effect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at mach numbers from 1.57 to 2.86

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:01:59Z
date available2017-09-04T17:01:59Z
date copyright01/01/1963
date issued1963
identifier otherXSTKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/125441
description abstractAfterbody geometry and sting diameter effect on aerodynamics of slender bodies at supersonic speed
languageEnglish
titleNASA-TN-D-2042num
titleEffect of afterbody geometry and sting diameter on the aerodynamic characteristics of slender bodies at mach numbers from 1.57 to 2.86en
typestandard
page32
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1963
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAERODYNAMICS
subject keywordsAFTERBODIES
subject keywordsAFTERBODY
subject keywordsBOATS
subject keywordsBODIES
subject keywordsBODY
subject keywordsCHARACTERISTICS
subject keywordsMACH
subject keywordsMOUNTING
subject keywordsNUMBER
subject keywordsSLENDER
subject keywordsSPEED
subject keywordsSUPERSONIC


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