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Fatigue Crack Closure Analysis Using Digital Image CorrelationFatigue crack closure during crack growth testing is analyzed in order to evaluate the critieria of ASTM Standard E647 for measurement of fatigue crack growth rates. Of specific concern is remote closure, which occurs away from the crack tip and is a product of the load history during crack-driving-force-reduction fatigue crack growth testing. Crack closure behavior is characterized using relative displacements determined from a series of high-magnification digital images acquired as the crack is loaded. Changes in the relative displacements of features on opposite sides of the crack are used to generate crack closure data as a function of crack wake position. For the results presented in this paper, remote closure did not affect fatigue crack growth rate measurements when ASTM Standard E647 was strictly followed and only became a problem when testing parameters (e.g., load shed rate, initial crack driving force, etc.) greatly exceeded the guidelines of the accepted standard.
Document ID
20100021172
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Leser, William P.
(North Carolina State Univ. Raleigh, NC, United States)
Newman, John A.
(NASA Langley Research Center Hampton, VA, United States)
Johnston, William M.
(Lockheed Martin Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Subject Category
Metals And Metallic Materials
Report/Patent Number
NF1676L-10554
NASA/TM-2010-216695
L-19865
Report Number: NF1676L-10554
Report Number: NASA/TM-2010-216695
Report Number: L-19865
Funding Number(s)
WBS: WBS 645846.02.07.07.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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