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NACA-TN-1473

High-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wing

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:19:57Z
date available2017-09-04T16:19:57Z
date copyright01/01/1947
date issued1947
identifier otherBLXSYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/83423
description abstractA high-speed wind-tunnel investigation was made of the aerodynamic characteristics at various Mach numbers of an NACA 65-210 semispan wing variously equipped with a 25-percent chord full-span slotted flap and 38-percent-semispan 20-percent-chord straight-saided aileron.
With the full-span flap retracted at a Mach number of 0.13, a maximum lift coefficient of 0.93 was obtained; and with the flap deflected 45°, a maximum lift coefficient of 1.87 was obtained.
languageEnglish
titleNACA-TN-1473num
titleHigh-speed wind-tunnel investigation of high lift and aileron-control characteristics of an NACA 65-210 semi-span wingen
typestandard
page33
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1947
contenttypefulltext
subject keywordsAILERONS
subject keywordsAIRFOILS
subject keywordsCARRIED
subject keywordsCHAR
subject keywordsDRAG
subject keywordsFLAPS
subject keywordsFULL
subject keywordsHIGH
subject keywordsHINGE
subject keywordsLMAL
subject keywordsLOW
subject keywordsMOMENTS
subject keywordsNACA
subject keywordsORDINATES
subject keywordsPARTIAL
subject keywordsROLLING
subject keywordsSLOTTED
subject keywordsSPAN
subject keywordsSPEED
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS
subject keywordsWORK
subject keywordsYAWING


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