NACA-RM-A7J22

High-speed aerodynamic characteristics of a model tail plane with modified NACA 65-010 sections and 0 degrees and 45 degrees sweepback

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:07:06Z
date available	2017-09-04T18:07:06Z
date copyright	01/01/1948
date issued	1948
identifier other	GOCTUDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/190057
description abstract	INTRODUCTION Recently, during recovery of an airplane from a high-speed dive, an unanticipated abrupt pitch-up and a large positive acceleration were encountered. (See reference 1.) In order to determine if the tail characteristics of this airplane were affected by Mach number, tests were made in Ames 16-foot high-speed wind tunnel of a semispan model of the horizontal tail plane of the airplane. The movable surface of the model tail plane is referred to in this report as a flap, for the results are applicable to other control surfaces. The aerodynamic characteristics of this model tail plane were measured with the flap hinge line unswept and swept back 45º.
language	English
title	NACA-RM-A7J22	num
title	High-speed aerodynamic characteristics of a model tail plane with modified NACA 65-010 sections and 0 degrees and 45 degrees sweepback	en
type	standard
page	88
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1948
contenttype	fulltext