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NASA-CR-413

Linear aerodynamic loads on cone-cylinders at Mach numbers from 0.7 to 2.0

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:44:48Z
date available2017-09-04T18:44:48Z
date copyright01/01/1966
date issued1966
identifier otherKFNKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=authoCA5893FD081D49A96159DD6EFDEC014A/handle/yse/226185
description abstractLinear aerodynamic loads for cone-cylinder configurations in trisonic range
languageEnglish
titleNASA-CR-413num
titleLinear aerodynamic loads on cone-cylinders at Mach numbers from 0.7 to 2.0en
typestandard
page88
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1966
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsCONE
subject keywordsCONES
subject keywordsCYLINDER
subject keywordsCYLINDERS
subject keywordsDISTRIBUTION
subject keywordsFORCES
subject keywordsLOAD
subject keywordsLOADS
subject keywordsSPEED
subject keywordsSUBSONIC
subject keywordsTRISONIC
subject keywordsTUNNELS
subject keywordsWIND


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