NACA-TN-2528

A method for predicting the upwash angles induced at the propeller plane of a combination of bodies with an upswept wing

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:28:57Z
date available	2017-09-04T16:28:57Z
date copyright	01/01/1951
date issued	1951
identifier other	UHLUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/92182
description abstract	A method has been developed the horizontal center line of the propeller disk of the twin-engine airplane considered in NACA TN 2192, 1950. The method treats each component separately and includes approximations for the interference effects of the other components. Lifting-line theory was used to determine the wing-induced upwash angles. The theory used for the nacelle is an extension of the airship theory of NACA TM 574, 1930. The fuselage-induced upwash angles were determined by means of a solution for the transverse flow about an infinite elliptic cylinder.
language	English
title	NACA-TN-2528	num
title	A method for predicting the upwash angles induced at the propeller plane of a combination of bodies with an upswept wing	en
type	standard
page	25
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1951
contenttype	fulltext