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NACA-TN-2741

Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:24:48Z
date available2017-09-04T15:24:48Z
date copyright01/01/1952
date issued1952
identifier otherNJLUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/25283
description abstractResults are presented of a wind-tunnel investigation to determine influence of the fuselage and tail on static stability and rotary derivatives in roll of a model having 45 degrees sweptback wing and tail surfaces. The wing alone and the model without the horizontal tail showed marginal longitudinal stability near maximum lift. The longitudinal stability of the complete model was satisfactory. The vertical tail produced larger increments of rate of change of lateral-force and yawing-moment coefficients with wing-tip helix angle than the fuselage or the horizontal tail.
languageEnglish
titleNACA-TN-2741num
titleInvestigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing modelen
typestandard
page19
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1952
contenttypefulltext
subject keywordsAIRPLANES
subject keywordsCOMBINATIONS
subject keywordsCOMPLETE
subject keywordsDAMPING
subject keywordsDERIVATIVES
subject keywordsFLOW
subject keywordsFUSELAGE
subject keywordsSTABILITY
subject keywordsSTATIC
subject keywordsSUBSONIC
subject keywordsSWEEP
subject keywordsTAIL
subject keywordsWING
subject keywordsWINGS


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