NACA-TN-182

Induced drag of multiplanes

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:23:22Z
date available	2017-09-04T15:23:22Z
date copyright	01/01/1924
date issued	1924
identifier other	NEYIYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/23581
description abstract	The most important part of the resistance or drag of a wing system,the induced drag, can be calculated theoretically, when the distribution of lift on the individual wings is known. The calculation is based upon the assumption that the lift on the wings is distributed along the wing in proportion to the ordinates of a semi-ellipse. Formulas and numerical tables are given for calculating the drag. In this connection, the most favorable arrangements of biplanes and triplanes are discussed and the results are further elucidated by means of numerical examples.
language	English
title	NACA-TN-182	num
title	Induced drag of multiplanes	en
type	standard
page	23
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1924
contenttype	fulltext