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NASA-TN-D-6283

A time-dependent method for calculating supersonic angle-of-attack flow about axisymmetric blunt bodies with sharp shoulders and smooth nonaxisymmetric blunt bodies

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:26:35Z
date available2017-09-04T18:26:35Z
date copyright01/01/1971
date issued1971
identifier otherILYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho47037D83FCDCAC42/handle/yse/208821
description abstractHypersonic and supersonic angle of attack flow about asymmetric and axisymmetric blunt bodies based on time dependent finite difference theory and method of characteristics
languageEnglish
titleNASA-TN-D-6283num
titleA time-dependent method for calculating supersonic angle-of-attack flow about axisymmetric blunt bodies with sharp shoulders and smooth nonaxisymmetric blunt bodiesen
typestandard
page76
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1971
contenttypefulltext
subject keywordsANGLE
subject keywordsASYMMETRY
subject keywordsATTACK
subject keywordsAXISYMMETRIC
subject keywordsBLUNT
subject keywordsBODIES
subject keywordsCHARACTERISTICS
subject keywordsDEPENDENCE
subject keywordsDIFFERENCE
subject keywordsDISTRIBUTION
subject keywordsFINITE
subject keywordsFLOW
subject keywordsHYPERSONIC
subject keywordsMETHOD
subject keywordsSUPERSONIC
subject keywordsTHEORY
subject keywordsTIME


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