titanium2: Titanium fatigue crack growth data

Description Format Source See Also

Description

A sample of 100 specimens of a titanium alloy were subjected to a fatigue test to determine time to crack initiation. The test was run up to a limit of 100,000 cycles. The observed number of cycles to crack initiation (in units of 1,000 of cycles) were: 18, 32, 39, 53, 59, 68, 77, 78, 93. No crack had initiated in any of the other 91 other specimens prior to reaching 100,000 cycles.

Format

A data.frame with 10 rows and 3 variables:

[, 1] kilocycles Accumulated cycles at event Numeric
[, 2] event Event observed at cycles (failure/right-censored) Categoric
[, 3] count Number of events observed at cycles Numeric

Source

Meeker, W. Q. and Escobar, L. A. (1998) Statistical Methods for Reliability Data, New York, NY; John Wiley & Sons.

Hudak, S.J., Saxena, A., Bucci, R. J., and Malcom, R .C. (1978), Development of standard methods of testing and analyzing fatigure crack growth rate data, Technical Report AFML-TR-78-40, Westinghouse R & D Center, Westinghouse Electric Corporation, Pittsburgh, PA.

See Also

Other data-notdone: adhesivebondc, adhesivestrength, amsaaexactfail, appliancea, applianceb, aprel72, atrazinejune, bearinga, censortruncationtest, chemicalprocess, cirpack4, cirpack5, componentd, concrete, connectionstrength, customerlife, devicedconnected, deviceh, devicen, diskber, doatrun, electromech, engineemissions, epoxyweathering, filament, hcfdata, heater, hpcrepairs, icdevice1, inconel, insulation, laminatepanel, largeball, locomotivecontrol, luminosity, machineh, mechanicalswitch, multiplefail, newspring, parta, piccioto, pipelinethickness, pmax(), prob3_5, riverchem, shelflifea, testdadtplan, titanium, tractorbreaks, turbinedevice, vehiclemotor, voltageendurance, workstation


Auburngrads/SMRD documentation built on Sept. 14, 2020, 2:21 a.m.