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A simple approximation method for obtaining the spanwise lift distribution

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:33:58Z
date available2017-09-04T17:33:58Z
date copyright01/01/1940
date issued1940
identifier otherDDYIYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/156789
description abstractThe approximation method described makes possible lift-distribution computations in a few minutes. Comparison with an exact method shows satisfactory agreement. The method is of greater applicability than the exact method and includes also the important case of the wing with end plates.
languageEnglish
titleNACA-TM-948num
titleA simple approximation method for obtaining the spanwise lift distributionen
typestandard
page16
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1940
contenttypefulltext


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