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Tests of related forward-camber airfoils in the variable-density wind tunnel

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:09:10Z
date available2017-09-04T18:09:10Z
date copyright01/01/1937
date issued1937
identifier otherGTWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/192233
description abstractA recent investigation of numerous related airfoils indicated that positions of camber forward of the usual location resulted in an increase of the maximum lift. As an extension of this investigation, a series of forward-camber airfoils has been developed, the members of which show airfoil characteristics superior to those of the airfoils previously investigated. The primary object of this report is to present fully corrected results for airfoils in the useful range of shapes. With the data thus made available, an airplane designer may intelligently choose the best possible airfoil-section shape for a given application and may predict to a reasonable degree the aerodynamic characteristics to be expected in flight from the section shape chosen.
languageEnglish
titleNACA-TR-610num
titleTests of related forward-camber airfoils in the variable-density wind tunnelen
typestandard
page42
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1937
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRFOIL
subject keywordsAIRFOILS
subject keywordsCAMBER
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsDRAG
subject keywordsEDGE
subject keywordsFLAPS
subject keywordsFULL
subject keywordsLIFT
subject keywordsPROFILES
subject keywordsRATIO
subject keywordsSCALE
subject keywordsSPLIT
subject keywordsTESTS
subject keywordsTHICKNESS
subject keywordsTRAILING
subject keywordsTUNNEL
subject keywordsWIND


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