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NACA-TR-611

Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:40:02Z
date available2017-09-04T18:40:02Z
date copyright01/01/1937
date issued1937
identifier otherJTWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=autho162sAF679D40AC421854DD6EFDEC9FCD/handle/yse/221761
description abstractReport presents the results of an investigation made in the NACA 7 by 10-foot wind tunnel to determine the aerodynamic properties of tapered wings having partial-span flaps for high lift and ordinary ailerons for lateral control. Each of two Clark-y wings, tapered 5:1 and 5:3, was equipped with partial-span split flaps of two lengths and with ordinary ailerons extending from the outboard ends of the flap to the wing tips. Measurements of wing forces and moments and of aileron hinge moments were made for the two conditions of flaps neutral and deflected.
languageEnglish
titleNACA-TR-611num
titleWind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flapsen
typestandard
page11
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1937
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAILERONS
subject keywordsCHARACTERISTICS
subject keywordsCONTROL
subject keywordsFLAPS
subject keywordsLATERAL
subject keywordsLIFT
subject keywordsMOMENTS
subject keywordsROLLING
subject keywordsSPLIT
subject keywordsSWEPT
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS
subject keywordsYAWING


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