Show simple item record

NASA-TM-X-1785

Jet effects on boattail pressure drag of isolated ejector nozzles at Mach numbers from 0.60 to 1.47

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:27:41Z
date available2017-09-04T16:27:41Z
date copyright01/01/1969
date issued1969
identifier otherUDNKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/90784
description abstractJet effects on boattail pressure drag of isolated ejector nozzles at Mach 0.60 to 1.47
languageEnglish
titleNASA-TM-X-1785num
titleJet effects on boattail pressure drag of isolated ejector nozzles at Mach numbers from 0.60 to 1.47en
typestandard
page91
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1969
contenttypefulltext
subject keywordsAIR
subject keywordsBOATTAILS
subject keywordsBOUNDARIES
subject keywordsBREATHING
subject keywordsDRAG
subject keywordsEJECTORS
subject keywordsENGINES
subject keywordsEXPANSION
subject keywordsFLOW
subject keywordsGAS
subject keywordsJET
subject keywordsNOZZLE
subject keywordsPRESSURE
subject keywordsSPEED
subject keywordsSUBSONIC


Files in this item

Thumbnail
Name:
UDNKAEAAAAAAAAAA.pdf
Size:
2.148Mb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record