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NACA-TR-669

Airfoil section data obtained in the N.A.C.A. variable-density tunnel as affected by support interference and other corrections

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1939

Abstract: The results of an investigation of the effect of support interference on airfoil drag data obtained in the variable-density tunnel are presented. As a result of the support interference, previously published airfoil data from the variable-density tunnel have shown too large drag coefficients and too large a rate of increase of drag coefficients and too large a rate increase of drag coefficients with airfoil thickness. The practical effect of the corrections on the choice of the optimum section is briefly considered and corrected data for a selected list of airfoils are presented as a convenience to the designer. Methods of correcting published data for other airfoils are presented.
URI: http://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/212544
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    NACA-TR-669

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:30:17Z
date available2017-09-04T18:30:17Z
date copyright01/01/1939
date issued1939
identifier otherIVWUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;query=author:%22NAVY%20-%206159DD6E273C9FCD0Facil/handle/yse/212544
description abstractThe results of an investigation of the effect of support interference on airfoil drag data obtained in the variable-density tunnel are presented. As a result of the support interference, previously published airfoil data from the variable-density tunnel have shown too large drag coefficients and too large a rate of increase of drag coefficients and too large a rate increase of drag coefficients with airfoil thickness. The practical effect of the corrections on the choice of the optimum section is briefly considered and corrected data for a selected list of airfoils are presented as a convenience to the designer. Methods of correcting published data for other airfoils are presented.
languageEnglish
titleNACA-TR-669num
titleAirfoil section data obtained in the N.A.C.A. variable-density tunnel as affected by support interference and other correctionsen
typestandard
page38
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1939
contenttypefulltext
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