NACA-TM-979

General airfoil theory

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:03:24Z
date available	2017-09-04T18:03:24Z
date copyright	01/01/1941
date issued	1941
identifier other	GDYIYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/186248
description abstract	On the assumption of infinitely small disturbances the author develops a generalized integral equation of airfoil theory which is applicable to any motion and compressible fluid. Successive specializations yield various simpler integral equations, such as Possio's, Birnbaum's, and Prandtl's integral equations, as well as new ones for the wing of infinite span with periodic downwash distribution and for the oscillating wing with high aspect ratio. Lastly, several solutions and methods for solving these integral equations are give.
language	English
title	NACA-TM-979	num
title	General airfoil theory	en
type	standard
page	29
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1941
contenttype	fulltext