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System for automated fatigue crack growth testing under random loading
Authors:R. Sunder
Affiliation:National Aeronautical Laboratory, Bangalore 560017, India
Abstract:Procedures have been developed for computer-controlled crack propagation testing under random load sequences. They include certain features which are not available in conventional systems, but which appear essential for random load testing. These include the capability to simulate any desired K-function on standard laboratory specimens and continuous on-line rainflow analysis of the test load sequence to exclude cycles falling below given values of threshold stress intensity, stress level or range. The system also includes a procedure for automated crack-opening displacement based crack opening/closing load level measurement. Experimental studies on AlCu alloy sheet material point to a requirement for development of standards for spectrum loading crack growth testing.
Keywords:fatigue  fatigue crack propagation  automated testing  random loading  cycle counting
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