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NASA-TN-D-3797

Large-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tail

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:32:34Z
date available2017-09-04T16:32:34Z
date copyright01/01/1967
date issued1967
identifier otherURYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/96051
description abstractStatic longitudinal stability and control at angles of attack above those for wing stall in large-scale subsonic transport model
languageEnglish
titleNASA-TN-D-3797num
titleLarge-scale wind tunnel tests of a subsonic transport with AFT engine nacelles and high tailen
typestandard
page49
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1967
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsANGLE
subject keywordsATTACK
subject keywordsCHARACTERISTICS
subject keywordsCONTROL
subject keywordsFUSELAGES
subject keywordsLONGITUDINAL
subject keywordsMODEL
subject keywordsMODELS
subject keywordsNACELLES
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsSTALLING
subject keywordsSTATIC
subject keywordsSUBSONIC
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND


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