NACA-CB-L5C01

Estimation of stick-fixed neutral points of airplanes

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:50:26Z
date available	2017-09-04T18:50:26Z
date copyright	01/01/1945
date issued	1945
identifier other	KUUYYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/231895
description abstract	A method is given for calculating the stick-fixed neutral point of an airplane with propeller windmilling, flaps neutral, and landing gear retracted. This method differs from those formerly used principally in the procedure for estimating the effect of the windmilling propeller. Comparison of the neutral points predicted by this method with neutral points obtained In flight tests indicates good agreement at low lift coefficients. The methods presented, in conjunction with the results given in NACA CB NQ.L4H01 "Effect of Power on the Stick-Fixed Neutral Points of Several Single-Engine Monoplanes as Determined in Flight," should be useful in estimating the stick-fixed neutral points of new designs for all flight conditions.
language	English
title	NACA-CB-L5C01	num
title	Estimation of stick-fixed neutral points of airplanes	en
type	standard
page	22
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1945
contenttype	fulltext