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REPORT DATE (DD-MM-YYYY)
30-12-2011
REPORT TYPE
Final Report
DATES COVERED
SPONSORING / MONITORING AGENCY NAME(S) AND ADDRESS(ES)Air Force Research Laboratory Space Vehicles Directorate 3550 Aberdeen Ave SE Kirtland AFB, NM 87117-5776
SPONSOR/MONITOR'S ACRONYM(S)AFRL/RVBYE
SPONSOR/MONITOR'S REPORT NUMBER(S)
AFRL-RV-PS-TR-2012-0035
DISTRIBUTION / AVAILABILITY STATEMENTApproved for public release; distribution is unlimited. (377ABW-2012-0113 dtd 01 Feb 2012)
SUPPLEMENTARY NOTES
ABSTRACTThe quasistatic damage mechanics formulated by Ashby and Sammis has been made fully dynamic by incorporating the results of recent experimental and theoretical studies of dynamic crack growth. The model has been verified by building it into the ABAQUS dynamic finite element code and using it to simulate high-speed fracture experiments. Simulation of explosions has shown that the spatial extent and pattern of the resultant fracture damage is sensitive to loading rate. High loading rates of short duration produce spherically symmetric compact damage patterns. Slower loading rates of longer duration are more effective in producing long radial fractures. Any asymmetry in the pattern of such radial fractures generates S wave radiation in the far-field, even in the absence of other factors known to generate S waves such as tectonic shear stress or anisotropy in the initial fracture distribution.
SUBJECT TERMSShear waves, Seismic sources, Model seismology, P and S wave radiation
SECURITY CLASSIFICATION OF:Fill in according to classification of report.