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NASA-TN-D-3845

Rolling stability derivatives of a variable-sweep tactical fighter model at subsonic and transonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:01:38Z
date available2017-09-04T17:01:38Z
date copyright01/01/1967
date issued1967
identifier otherXRYKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/125152
description abstractRolling stability derivatives of variable sweep tactical fighter aircraft model at subsonic and transonic speeds
languageEnglish
titleNASA-TN-D-3845num
titleRolling stability derivatives of a variable-sweep tactical fighter model at subsonic and transonic speedsen
typestandard
page57
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1967
contenttypefulltext
subject keywordsAIRCRAFT
subject keywordsANGLE
subject keywordsATTACK
subject keywordsDERIVATIVES
subject keywordsFIGHTER
subject keywordsMACH
subject keywordsMODELS
subject keywordsNUMBER
subject keywordsREYNOLDS
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsSUBSONIC
subject keywordsSWEEP
subject keywordsTRANSONIC
subject keywordsVARIABLE
subject keywordsWINGS


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