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NASA-TN-D-5102

Large-scale tests of an airplane model with a double-delta wing, including longitudinal and lateral characteristics and ground effects

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:19:20Z
date available2017-09-04T16:19:20Z
date copyright01/01/1969
date issued1969
identifier otherTHYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/82804
description abstractAerodynamic characteristics and ground effects of supersonic transport with double delta wing
languageEnglish
titleNASA-TN-D-5102num
titleLarge-scale tests of an airplane model with a double-delta wing, including longitudinal and lateral characteristics and ground effectsen
typestandard
page83
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1969
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAERODYNAMICS
subject keywordsANGLE
subject keywordsATTACK
subject keywordsCHARACTERISTICS
subject keywordsDELTA
subject keywordsDRAG
subject keywordsEFFECT
subject keywordsGROUND
subject keywordsLIFT
subject keywordsMODELS
subject keywordsRATIO
subject keywordsSTABILITY
subject keywordsSUPERSONIC
subject keywordsTESTS
subject keywordsTRANSPORTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWINGS


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