| crack | R Documentation |
Experimental fatigue crack length measurements on 21 alloy specimens subjected to cyclic stress testing up to 0.12 million cycles (120 thousand cycles).
crack
A data frame with 262 rows and 6 variables:
Integer specimen identifier (1 to 21).
Inspection time in millions of cycles (0.00 to 0.12).
Inspection time in cycles (0 to 120,000).
Inspection time in thousands of cycles (0 to 120).
Crack length measurement in inches (initial crack 0.90 inches, failure at 1.60 inches).
Transformed cumulative degradation D^*(t) = \log(D(t) / 0.90), with failure threshold \rho = 0.5754.
Lu, C. J., & Meeker, W. Q. (1993). Using degradation measures to estimate a time-to-failure distribution. Technometrics, 35(2), 161-174. \Sexpr[results=rd]{tools:::Rd_expr_doi("10.1080/00401706.1993.10485038")}.
Morita, L. H. M., Tomazella, V. L. D., Balakrishnan, N., Ramos, P. L., Ferreira, P. H., & Louzada, F. (2021). Inverse Gaussian process model with frailty term in reliability analysis. Quality and Reliability Engineering International, 37(2), 763-784. \Sexpr[results=rd]{tools:::Rd_expr_doi("10.1002/qre.2762")}.
data(crack)
head(crack)
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