NACA-TN-1525

Stress And Distortion Measurements in A 45 Degrees Swept Box Beam subjected to Bending and to Torsion

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:13:01Z
date available	2017-09-04T18:13:01Z
date copyright	03/01/1948
date issued	1948
identifier other	HDYHUEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/196014
description abstract	Present designs of aircraft fro transonic speeds call for wings with large angles of sweep. In order to study the structural problems encountered in the design of swept wings a 45 degrees swept box beam, shown in figures 1 and 2, was subjected to symmetrical tip loading and its stresses and distortions were measured. This paper gives the measured data and compared the stresses with those given by standard beam formulas and the distortions with those estimated on the basis of approximate calculations.
language	English
title	NACA-TN-1525	num
title	Stress And Distortion Measurements in A 45 Degrees Swept Box Beam subjected to Bending and to Torsion	en
type	standard
page	42
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1948
contenttype	fulltext
subject keywords	BEAMS
subject keywords	BOX - BENDING & TORSION
subject keywords	BEAMS
subject keywords	BOX - STRESSES
subject keywords	BEAMS
subject keywords	CANTILEVER - STRESSES
subject keywords	LOADS - BEAMS
subject keywords	BOX
subject keywords	STRESSED SKIN - BEAMS BOX
subject keywords	WING SPARS - DEFLECTION
subject keywords	WING SPARS
subject keywords	BOX - BENDING & TORSION
subject keywords	WING
subject keywords	SWEPTBACK