NACA-TR-540

Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:54:21Z
date available	2017-09-04T15:54:21Z
date copyright	01/01/1936
date issued	1936
identifier other	QRWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/57654
description abstract	This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number.
language	English
title	NACA-TR-540	num
title	Interference of wing and fuselage from tests of 209 combinations in the NACA variable-density tunnel	en
type	standard
page	44
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1936
contenttype	fulltext