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NACA-TN-3346

Prediction of downwash behind swept-wing airplanes at subsonic speed

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

Abstract: A rapid method for estimating the downwash behind swept-wing airplanes is presented. The basic assumption is that of a flat horizontal sheet of vortices trailing behind the wing. The integrations for the downwash are handled in a manner similar to both Multhopp's and Weissinger's approximate integrations in their span-loading calculations. The principal effects of rolling-up of the wake are treated as corrections to the flat-sheet wake. A simple approximate correction for the effect of the fuselage is applied. The agreement with available experimental data taken behind airplane models is good. Computing forms are included together with charts of pertinent functions, so as to enable simple direct application.
URI: http://yse.yabesh.ir/std/handle/yse/231786
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    NACA-TN-3346

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:50:21Z
date available2017-09-04T18:50:21Z
date copyright01/01/1955
date issued1955
identifier otherKUNUYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/231786
description abstractA rapid method for estimating the downwash behind swept-wing airplanes is presented. The basic assumption is that of a flat horizontal sheet of vortices trailing behind the wing. The integrations for the downwash are handled in a manner similar to both Multhopp's and Weissinger's approximate integrations in their span-loading calculations. The principal effects of rolling-up of the wake are treated as corrections to the flat-sheet wake. A simple approximate correction for the effect of the fuselage is applied. The agreement with available experimental data taken behind airplane models is good. Computing forms are included together with charts of pertinent functions, so as to enable simple direct application.
languageEnglish
titleNACA-TN-3346num
titlePrediction of downwash behind swept-wing airplanes at subsonic speeden
typestandard
page105
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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