NACA-TN-4146

Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:48:16Z
date available	2017-09-04T15:48:16Z
date copyright	01/01/1958
date issued	1958
identifier other	QAOUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/51161
description abstract	A wind-tunnel investigation was conducted at a Mach number of 1.96 and at Reynolds numbers (based on the mean aerodynamic chord of the exposed wing) of 0.36 and 1.03 minion to determine the normal forces pitching moments, and rolling moments contributed by each wing panel of a cruciform-wing and body combination over a wide range of combined angles of pitch and roll. The wings were triangular of aspect ratio 2, and the body was an ogive-cyldnder combination. The effects of forebody length and roughness and of the presence of the adjacent panels on these panel contributions were determined.
language	English
title	NACA-TN-4146	num
title	Contribution of the wing panels to the forces and moments of supersonic wing-body combinations at combined angles	en
type	standard
page	64
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1958
contenttype	fulltext