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NASA-TM-X-72843

Effects of thickness on the aerodynamic characteristics of an initial low-speed family of airfoils for general aviation applications

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:08:05Z
date available2017-09-04T18:08:05Z
date copyright01/01/1976
date issued1976
identifier otherGQTKAEAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/191030
description abstractWind tunnel tests were conducted to determine the effects of airfoil thickness-ratio on the low speed aerodynamic characteristics of an initial family of airfoils. The results were compared with theoretical predictions obtained from a subsonic viscous method. The tests were conducted over a Mach number range from 0.10 to 0.28. Chord Reynolds numbers varied from about 2.0 x 1 million to 9.0 x 1 million.
languageEnglish
titleNASA-TM-X-72843num
titleEffects of thickness on the aerodynamic characteristics of an initial low-speed family of airfoils for general aviation applicationsen
typestandard
page54
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1976
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsAIRFOILS
subject keywordsAVIATION
subject keywordsCHARACTERISTICS
subject keywordsFLOW
subject keywordsGENERAL
subject keywordsLOW
subject keywordsMACH
subject keywordsNUMBER
subject keywordsRATIO
subject keywordsREYNOLDS
subject keywordsSPEED
subject keywordsTESTS
subject keywordsTHICKNESS
subject keywordsTUNNEL
subject keywordsVISCOUS
subject keywordsWIND


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