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NACA-TN-2229

The effect of end plates on swept wings at low speed

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:41:38Z
date available2017-09-04T15:41:38Z
date copyright01/01/1950
date issued1950
identifier otherPHEUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/43902
description abstractAn investigation was made in the Langley 300 MPH 7. by 10-foot tunnel to determine the effects of various sizes end shapes of end plates on the aileron characteristics and on the aerodynamic characteristics in pitch end yaw of a wing of aspect ratio 2 with no taper and a sweepback of 45° and of a wing of aspect ratio 4, taper ratio 0.6, and sweepback of 46.7°. Free-roll characteristics were obtained with two end-plate configurations on a wing of aspect ratio 3, taper ratio 0.6, and a sweepback of 35° in order to determine the effect of end plates on wing damping in roll.
languageEnglish
titleNACA-TN-2229num
titleThe effect of end plates on swept wings at low speeden
typestandard
page61
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1950
contenttypefulltext
subject keywordsAILERONS
subject keywordsCHARACTERISTICS
subject keywordsDIHEDRAL
subject keywordsEND
subject keywordsFEET
subject keywordsMPH
subject keywordsNACA
subject keywordsPLATES
subject keywordsSPOILER
subject keywordsSTABILITY
subject keywordsSWEPTBACK
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWINGS


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