NACA-TN-640

Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel - combination with split flaps

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:22:55Z
date available	2017-09-04T18:22:55Z
date copyright	01/01/1938
date issued	1938
identifier other	AGYIYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/205339
description abstract	As part of the wing-fuselage interference investigation in progress in the N.A.C.A. variable density wind tunnel, the effects of various split-flap arrangements applied to wing-fuselage combinations were determined. Split flaps were found to exert their influence independently of the interference, and their effects on the aerodynamic characteristics of rectangular-airfoil combinations appeared to be more or less proportional to their exposed span lengths. The interference, moreover, showed the same character with the split flaps as without them.
language	English
title	NACA-TN-640	num
title	Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel - combination with split flaps	en
type	standard
page	17
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1938
contenttype	fulltext