Fatigue Crack Growth Measurement and Data Analysis
Author: S. J. Hudak
Publisher: ASTM International
Published: 1981
Total Pages: 384
ISBN-13: 9780803107175
DOWNLOAD EBOOK →Author: S. J. Hudak
Publisher: ASTM International
Published: 1981
Total Pages: 384
ISBN-13: 9780803107175
DOWNLOAD EBOOK →Author: S. J Hudak
Publisher: ASTM International
Published: 1981
Total Pages: 374
ISBN-13:
DOWNLOAD EBOOK →Author: W. H. Cullen
Publisher: ASTM International
Published: 1985
Total Pages: 316
ISBN-13: 9780803104211
DOWNLOAD EBOOK →Author: J. C. Newman
Publisher: ASTM International
Published: 2000
Total Pages: 436
ISBN-13: 0803126247
DOWNLOAD EBOOK →Annotation Contains 24 papers from the November, 1998 symposium of the same name, sponsored by the ASTM Committee E8 on Fatigue and Fracture, and presented by Newman and Piascik (both of the NASA Langley Research Center). The papers focus on such areas as fatigue-crack growth threshold mechanisms, loading and specimen-type effects, analyses of fatigue-crack-growth-threshold behavior, and applications of threshold concepts and endurance limits to aerospace and structural materials. Annotation copyrighted by Book News, Inc., Portland, OR.
Author: R. Craig McClung
Publisher: ASTM International
Published: 1999
Total Pages: 487
ISBN-13: 0803126115
DOWNLOAD EBOOK →Author: J. N. Yang
Publisher:
Published: 1985
Total Pages: 268
ISBN-13:
DOWNLOAD EBOOK →Various stochastic models for fatigue crack propagation under either constant amplitude or spectrum loadings have been investigated. These models are based on the assumption that the crack growth rate is a lognormal random process, including the general lognormal random process, lognormal white noise process, lognormal random variable, and second moment approximations, such as Weibull, gamma, lognormal and Gaussian closure approximations. Extensive experimental data have been used for the correlation study with various stochastic models. These include fastener hole specimens under fighter or bomber spectrum laodings and center-cracked specimens under constant amplitude loads. The data sets for the fastener hole specimens cover adequately different loading conditions, environments, load transfers and crack size range. It is shown that the white noise process is definitely not a valid model for fatigue crack propagation.