NACA-TR-650

The aerodynamic characteristics of six full-scale propellers having different airfoil sections

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:55:20Z
date available	2017-09-04T15:55:20Z
date copyright	01/01/1939
date issued	1939
identifier other	QUWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/58728
description abstract	Wind-tunnel tests are reported of six 3-blade 10-foot propellers operated in front of a liquid-cooled engine nacelle. The propellers were identical except for blade airfoil sections, which were: Clark y, R.A.F. 6, NACA 4400, NACA 2400-34, NACA 2rsub200, and NACA 6400. The range of blade angles investigated extended for 15 degrees to 40 degrees for all propellers except the Clark y, for which it extended to 45 degrees. The results showed that the range in maximum efficiency between the highest and lowest values was about 3 percent. The highest efficiencies were for the low-camber sections.
language	English
title	NACA-TR-650	num
title	The aerodynamic characteristics of six full-scale propellers having different airfoil sections	en
type	standard
page	56
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1939
contenttype	fulltext