NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
The Purpose of Generating Fatigue Crack Growth Threshold DataTest data shows that different width and thickness C(T), M(T) and ESE(T) specimens generate different thresholds Structures designed for "infinite life" are being re-evaluated: a) Threshold changes from 6 to 3 ksi in(sup 1/2); b) Computational life changes from infinite to 4 missions. Multi-million dollar test programs required to substantiate operation. Using ASTM E647 as standard guidance to generate threshold data is not practical. A threshold test approach needs to be standardized that will provide positive margin for high cycle fatigue applications.
Document ID
20080031625
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Forth, Scott
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 24, 2013
Publication Date
November 13, 2006
Subject Category
Structural Mechanics
Meeting Information
Meeting: ASTM Committee Meeting
Location: Atlanta, GA
Country: United States
Start Date: November 13, 2006
End Date: November 16, 2006
Sponsors: ASTM International
Funding Number(s)
WBS: WBS 981155.01.05.12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available