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NACA-RM-A54J20

Effect of taper ratio on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 with 53.1 degrees sweepback of leading edge at subsonic and supersonic speeds

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NASA - National Aeronautics and Space Administration (NASA)
Year: 1955

Abstract: INTRODUCTION
As part of the continuing investigation of low-aspect-ratio wings by the NACA, the effects of taper ratio on the aerodynamic characteristics of swept wings of aspect ratio 3 at subsonic and supersonic speeds have been investigated in the Ames 6- by 6-foot supersonic wind tunnel. This report is devoted to the presentation and discussion of the results obtained during this study.
URI: https://yse.yabesh.ir/std/handle/yse/101681
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    NACA-RM-A54J20

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:38:06Z
date available2017-09-04T16:38:06Z
date copyright01/01/1955
date issued1955
identifier otherVHMCWDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/101681
description abstractINTRODUCTION
As part of the continuing investigation of low-aspect-ratio wings by the NACA, the effects of taper ratio on the aerodynamic characteristics of swept wings of aspect ratio 3 at subsonic and supersonic speeds have been investigated in the Ames 6- by 6-foot supersonic wind tunnel. This report is devoted to the presentation and discussion of the results obtained during this study.
languageEnglish
titleNACA-RM-A54J20num
titleEffect of taper ratio on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 with 53.1 degrees sweepback of leading edge at subsonic and supersonic speedsen
typestandard
page26
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
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