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NACA-TR-628

Aerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnel

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1938

Abstract: airfoils tested in the variable-density tunnel have been reduced to a comparable form and are published in this report for convenient reference. Plots of the standard characteristics are given in tabular form. Included is a tabulation of important characteristics for the related airfoils reported in NACA report 460. This report, in conjunction with NACA report 610, makes available in comparable and convenient form the aerodynamic data for airfoils tested in the variable-density tunnel since January 1, 1931.
URI: https://yse.yabesh.ir/std/handle/yse/48628
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    NACA-TR-628

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:45:59Z
date available2017-09-04T15:45:59Z
date copyright01/01/1938
date issued1938
identifier otherPTWUYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/48628
description abstractairfoils tested in the variable-density tunnel have been reduced to a comparable form and are published in this report for convenient reference. Plots of the standard characteristics are given in tabular form. Included is a tabulation of important characteristics for the related airfoils reported in NACA report 460. This report, in conjunction with NACA report 610, makes available in comparable and convenient form the aerodynamic data for airfoils tested in the variable-density tunnel since January 1, 1931.
languageEnglish
titleNACA-TR-628num
titleAerodynamic characteristics of a large number of airfoils tested in the variable-density wind tunnelen
typestandard
page56
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1938
contenttypefulltext
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