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NASA-TN-D-4563

Calculation of axisymmetric supersonic flow past blunt bodies with sonic corners, including a program description and listing

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:08:51Z
date available2017-09-04T18:08:51Z
date copyright01/01/1968
date issued1968
identifier otherGSYKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/191887
description abstractFORTRAN program for approximate calculation of supersonic ideal gas flow past blunt bodies with sonic corners
languageEnglish
titleNASA-TN-D-4563num
titleCalculation of axisymmetric supersonic flow past blunt bodies with sonic corners, including a program description and listingen
typestandard
page65
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1968
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANALYSIS
subject keywordsAPPROXIMATION
subject keywordsBLUNT
subject keywordsBODIES
subject keywordsCHARACTERISTICS
subject keywordsCOMPUTER
subject keywordsCORNERS
subject keywordsFLOW
subject keywordsFORTRAN
subject keywordsGAS
subject keywordsIDEAL
subject keywordsNUMERICAL
subject keywordsPROGRAMS
subject keywordsSUPERSONIC
subject keywordsTRANSONIC


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