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NASA-TM-X-72697

Low-speed aerodynamic characteristics of a 13-percent-thick airfoil section designed for general aviation applications

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:30:47Z
date available2017-09-04T15:30:47Z
date copyright01/01/1975
date issued1975
identifier otherAWTKAEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/32235
description abstractWind-tunnel tests were conducted to determine the low-speed section characteristics of a 13 percent-thick airfoil designed for general aviation applications. The results were compared with NACA 12 percent-thick sections and with the 17 percent-thick NASA airfoil. The tests were conducted ovar a Mach number range from 0.10 to 0.35. Chord Reynolds numbers varied from about 2,000,000 to 9,000,000.
languageEnglish
titleNASA-TM-X-72697num
titleLow-speed aerodynamic characteristics of a 13-percent-thick airfoil section designed for general aviation applicationsen
typestandard
page58
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1975
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsAIRFOIL
subject keywordsAVIATION
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsGENERAL
subject keywordsLOW
subject keywordsMODELS
subject keywordsNUMBER
subject keywordsPROFILES
subject keywordsREYNOLDS
subject keywordsSPEED
subject keywordsSTABILITY
subject keywordsTESTS
subject keywordsTUNNEL
subject keywordsWIND


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