NACA-TN-3501

The transonic characteristics of 22 rectangular, symmetrical wing models of varying aspect ratio and thickness

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:05:13Z
date available	2017-09-04T16:05:13Z
date copyright	01/01/1955
date issued	1955
identifier other	RVNUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/68509
description abstract	An investigation to determine the aerodynamic characteristics of a series of thin, rectangular wings was conducted in the Ames 16-foot high-speed wind tunnel, utilizing the transonic bump technique over a mach number range from 0.40 to 1.10, corresponding to a Reynolds number range from 1.25 to 2.05 million. The lift, drag, and pitching-moment data are presented for wings having aspect ratios of 6, 4, 3, 2, 1.5, 1, and 0.5, and NACA 63AOXX sections with thickness-to-chord ratios of 10,8,6,4, and 2 percent.
language	English
title	NACA-TN-3501	num
title	The transonic characteristics of 22 rectangular, symmetrical wing models of varying aspect ratio and thickness	en
type	standard
page	110
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1955
contenttype	fulltext