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NASA-TM-X-35

Effects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:15:10Z
date available2017-09-04T17:15:10Z
date copyright01/01/1960
date issued1960
identifier otherZCNKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/138604
description abstractVertical tail size and ventral fin effects on lateral and directional stability of VTOL AIRCRAFT at transonic speeds
languageEnglish
titleNASA-TM-X-35num
titleEffects of vertical-tail size and a ventral fin on the static lateral and directional stability derivatives of a 0.048-scale model of a horizontal-attitude VTOL airplane at transonic speedsen
typestandard
page57
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsAIRCRAFT
subject keywordsAIRSPEED
subject keywordsANGLE
subject keywordsASSEMBLIES
subject keywordsATTACK
subject keywordsDERIVATIVES
subject keywordsDIRECTIONAL
subject keywordsDYNAMICS
subject keywordsFINS
subject keywordsFLUID
subject keywordsLATERAL
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsSTABILIZERS
subject keywordsSTATIC
subject keywordsTAIL
subject keywordsTAKEOFF
subject keywordsTRANSONIC
subject keywordsVERTICAL
subject keywordsVTOL


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