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NACA-TN-1773

The effects of variations in Reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

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NASA - National Aeronautics and Space Administration (NASA)
Year: 1948

Abstract: Results are presented of an investigation made to determine the two dimensional lift and drag characteristics of nine naca 6-series airfoil sections at Reynolds numbers of 15.0x106, 20.0x106, and 25.0x106. Also presented are data from NACA Rep. No. 824 for the same airfoils at Reynolds number of 3.0x106, 6.0x106. The airfoils selected represent sections haying variations in the airfoil thickness, split flap were determined in one instance, as was the effect of surface roughness. Qualitative explanations in terms of flow behavior are advanced for the observed types of scale effect.
URI: https://yse.yabesh.ir/std/handle/yse/3655
Subject: AIRFOILS
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  • NASA - National Aeronautics and Space Administration (NASA)
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    NACA-TN-1773

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:06:08Z
date available2017-09-04T15:06:08Z
date copyright01/01/1948
date issued1948
identifier otherLDYTYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/3655
description abstractResults are presented of an investigation made to determine the two dimensional lift and drag characteristics of nine naca 6-series airfoil sections at Reynolds numbers of 15.0x106, 20.0x106, and 25.0x106. Also presented are data from NACA Rep. No. 824 for the same airfoils at Reynolds number of 3.0x106, 6.0x106. The airfoils selected represent sections haying variations in the airfoil thickness, split flap were determined in one instance, as was the effect of surface roughness. Qualitative explanations in terms of flow behavior are advanced for the observed types of scale effect.
languageEnglish
titleNACA-TN-1773num
titleThe effects of variations in Reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sectionsen
typestandard
page43
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1948
contenttypefulltext
subject keywordsAIRFOILS
subject keywordsCHAR
subject keywordsNACA
subject keywordsNUMBER
subject keywordsORDINATES
subject keywordsREYNOLDS
subject keywordsSERIES
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