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NACA-TN-3963

A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1957

Abstract: The low-speed stalling characteristics of a large number of airfoil sections have been correlated with Reynolds number and a single airfoil ordinate near the leading edge as the correlating parameters. The correlation is appropriate only to airfoils without high-lift devices in flows of very low turbulence and with aerodynamically smooth surfaces.
URI: https://yse.yabesh.ir/std/handle/yse/108708
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    NACA-TN-3963

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:45:25Z
date available2017-09-04T16:45:25Z
date copyright01/01/1957
date issued1957
identifier otherVZNUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/108708
description abstractThe low-speed stalling characteristics of a large number of airfoil sections have been correlated with Reynolds number and a single airfoil ordinate near the leading edge as the correlating parameters. The correlation is appropriate only to airfoils without high-lift devices in flows of very low turbulence and with aerodynamically smooth surfaces.
languageEnglish
titleNACA-TN-3963num
titleA correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometryen
typestandard
page10
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1957
contenttypefulltext
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