NACA-RM-L8G05

Full-scale investigation of an equilateral triangular wing having 10-percent-thick biconvex airfoil sections

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:04:59Z
date available	2017-09-04T16:04:59Z
date copyright	01/01/1948
date issued	1948
identifier other	RUSWXDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/68228
description abstract	INTRODUCTION A wing having triangular plan form, 60° of sweepback at the leading edge, and 10-percent-tuck biconvex airfoil sections has been tested in the Langley full-scale tunnel as part of a general investigation of the low-speed characteristics of probable hi&-speed-airplane configurations. The investigation included tests to determine the effects of semispan and f full-span leading edge and trailing-edge flaps on the longitudinal aerodynamic characteristics of the triangular wing. Tests were made of several leading-edge and trailing-edge flap combinations to determine the optimum low-speed flap configuration. The lateral Characteristics of the unflapped triangular. wing, with and without a Vertical fin installed, were also determined.
language	English
title	NACA-RM-L8G05	num
title	Full-scale investigation of an equilateral triangular wing having 10-percent-thick biconvex airfoil sections	en
type	standard
page	36
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1948
contenttype	fulltext