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NASA-TM-X-1658

Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:31:22Z
date available2017-09-04T15:31:22Z
date copyright01/01/1968
date issued1968
identifier otherODNKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/32901
description abstractAerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg
languageEnglish
titleNASA-TM-X-1658num
titleAerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 degen
typestandard
page41
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1968
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsATTACK
subject keywordsBODIES
subject keywordsCENTER
subject keywordsCHARACTERISTICS
subject keywordsDESCENT
subject keywordsFINENESS
subject keywordsFOREBODIES
subject keywordsGRAVITY
subject keywordsLONGITUDINAL
subject keywordsNOSES
subject keywordsNUMBER
subject keywordsPARACHUTE
subject keywordsPAYLOADS
subject keywordsRATIO
subject keywordsREVOLUTION
subject keywordsREYNOLDS
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsSUPERSONIC
subject keywordsTUNNELS
subject keywordsWIND


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