NASA-TN-D-1259

Unified Notch-Strength Analysis for Wrought Aluminum Alloys

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:32:48Z
date available	2017-09-04T15:32:48Z
date copyright	05/01/1962
date issued	1962
identifier other	OHYHUEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std/handle/yse/34468
description abstract	A simple engineering method is presented for predicting the strength of notched parts made from wrought aluminum alloys under static loading or under repeated loading near the fatigue limit. Assumed to be known are tensile strength, elongation and modulus of elasticity; in certain cases, the stress-strain curve must be known; also needed are "Neuber constants," which are given in the report. Notch configurations ranging from mild notches to cracks are considered. A large number of comparisons between experimental and predicted results are presented.
language	English
title	NASA-TN-D-1259	num
title	Unified Notch-Strength Analysis for Wrought Aluminum Alloys	en
type	standard
page	84
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1962
contenttype	fulltext
subject keywords	ALUMINUM ALLOY
subject keywords	ALUMINUM ALLOYS
subject keywords	CRACKS
subject keywords	ELONGATION
subject keywords	MODULUS OF ELASTICITY
subject keywords	NOTCH STRENGTH
subject keywords	STATIC LOADS
subject keywords	STRESS-STRAIN DIAGRAMS
subject keywords	TENSILE PROPERTIES
subject keywords	WROUGHT ALLOY
subject keywords	WROUGHT ALLOYS