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NACA-TN-1677

Experimental and calculated characteristics of several high-aspect-ratio tapered wings incorporating NACA 44-series, 230-series, and low-drag 64-series airfoil sections

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:30:32Z
date available2017-09-04T15:30:32Z
date copyright01/01/1948
date issued1948
identifier otherOAVTYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/31917
description abstractThe lift, drag, and pitching-moment characteristics of several unswept wings were determined by wind-tunnel tests and by calculations using the method of NACA tn no. 1269. The wings were similar in plan from with aspect ratio 10, taper ratio 2.5 and with root-chord and tip-chord thickness ratios of 20 and 12 percent, respectively. The airfoil sections used were the NACA 44-series, 230-series, and low-drag 64-series.
languageEnglish
titleNACA-TN-1677num
titleExperimental and calculated characteristics of several high-aspect-ratio tapered wings incorporating NACA 44-series, 230-series, and low-drag 64-series airfoil sectionsen
typestandard
page39
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1948
contenttypefulltext
subject keywordsAIRFOILS
subject keywordsASPECT
subject keywordsCARRIED
subject keywordsCHARACTERISTICS
subject keywordsDRAG
subject keywordsEFFECT
subject keywordsFLAPS
subject keywordsLAL
subject keywordsLARGE
subject keywordsLOW
subject keywordsMOMENTS
subject keywordsNACA
subject keywordsPITCHING
subject keywordsPRESSURE
subject keywordsRATIO
subject keywordsROUGHNESS
subject keywordsSPLIT
subject keywordsSTALLING
subject keywordsSURFACE
subject keywordsTAPERED
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND
subject keywordsWING
subject keywordsWINGS
subject keywordsWORK


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