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NASA-TM-X-213

Investigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:53:02Z
date available2017-09-04T17:53:02Z
date copyright01/01/1960
date issued1960
identifier otherFDNKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/176237
description abstractDrag and static longitudinal and lateral stability characteristics of supersonic horizontal attitude VTOL aircraft model in wind tunnel
languageEnglish
titleNASA-TM-X-213num
titleInvestigation of the aerodynamic characteristics of a supersonic horizontal- attitude VTOL airplane model at Mach numbers of 1.57, 2.14, 2.54, and 2.87en
typestandard
page155
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsATTITUDE
subject keywordsCHARACTERISTICS
subject keywordsDRAG
subject keywordsINCLINATION
subject keywordsLATERAL
subject keywordsLONGITUDINAL
subject keywordsMACH
subject keywordsMODEL
subject keywordsMODELS
subject keywordsNUMBER
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSUPERSONIC
subject keywordsTAKEOFF
subject keywordsTUNNEL
subject keywordsVERTICAL
subject keywordsVTOL
subject keywordsWIND


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