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
Environmental fatigue of an Al-Li-Cu alloy. Part 3: Modeling of crack tip hydrogen damageEnvironmental fatigue crack propagation rates and microscopic damage modes in Al-Li-Cu alloy 2090 (Parts 1 and 2) are described by a crack tip process zone model based on hydrogen embrittlement. Da/dN sub ENV equates to discontinuous crack advance over a distance, delta a, determined by dislocation transport of dissolved hydrogen at plastic strains above a critical value; and to the number of load cycles, delta N, required to hydrogenate process zone trap sites that fracture according to a local hydrogen concentration-tensile stress criterion. Transgranular (100) cracking occurs for process zones smaller than the subgrain size, and due to lattice decohesion or hydride formation. Intersubgranular cracking dominates when the process zone encompasses one or more subgrains so that dislocation transport provides hydrogen to strong boundary trapping sites. Multi-sloped log da/dN-log delta K behavior is produced by process zone plastic strain-hydrogen-microstructure interactions, and is determined by the DK dependent rates and proportions of each parallel cracking mode. Absolute values of the exponents and the preexponential coefficients are not predictable; however, fractographic measurements theta sub i coupled with fatigue crack propagation data for alloy 2090 established that the process zone model correctly describes fatigue crack propagation kinetics. Crack surface films hinder hydrogen uptake and reduce da/dN and alter the proportions of each fatigue crack propagation mode.
Document ID
19920021971
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Piascik, Robert S.
(NASA Langley Research Center Hampton, VA, United States)
Gangloff, Richard P.
(Virginia Univ. Charlottesville., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-107619
NAS 1.15:107619
Report Number: NASA-TM-107619
Report Number: NAS 1.15:107619
Accession Number
92N31215
Funding Number(s)
PROJECT: RTOP 505-63-50-04
CONTRACT_GRANT: NAG1-745
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available