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7075-T6 and 2024-T351 Aluminum Alloy Fatigue Crack Growth Rate DataExperimental test procedures for the development of fatigue crack growth rate data has been standardized by the American Society for Testing and Materials. Over the past 30 years several gradual changes have been made to the standard without rigorous assessment of the affect these changes have on the precision or variability of the data generated. Therefore, the ASTM committee on fatigue crack growth has initiated an international round robin test program to assess the precision and variability of test results generated using the standard E647-00. Crack growth rate data presented in this report, in support of the ASTM roundrobin, shows excellent precision and repeatability.
Document ID
20050215293
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Forth, Scott C.
(NASA Langley Research Center Hampton, VA, United States)
Wright, Christopher W.
(NASA Langley Research Center Hampton, VA, United States)
Johnston, William M., Jr.
(Lockheed Martin Corp. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2005
Subject Category
Metals And Metallic Materials
Report/Patent Number
L-19163
NASA/TM-2005-213907
Report Number: L-19163
Report Number: NASA/TM-2005-213907
Funding Number(s)
WORK_UNIT: WU 23-064-30-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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