NACA-TM-910

Measurements on a low-wing model in the rotating jet and comparison with flight measurements

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:11:26Z
date available	2017-09-04T18:11:26Z
date copyright	01/01/1939
date issued	1939
identifier other	ADYIYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/194417
description abstract	The present report deals with six-component measurements in the small tunnel of the DVL on a model of the BFW-M 27b(sub 1), which were made to determine the effect of rolling and yawing on the air forces and moments. The wind was given a spiral motion by means of a rotating screen, the model being suspended in the conventional manner.
language	English
title	NACA-TM-910	num
title	Measurements on a low-wing model in the rotating jet and comparison with flight measurements	en
type	standard
page	21
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1939
contenttype	fulltext