Failure Criterion for Isotropic Time Dependent Materials Which Accounts for Multi-Axial Loading

摘要

The Space Shuttle's Reusable Solid Rocket Motor (RSRM) nozzle program has recently conducted testing to characterize the effects of multi-axial loading, temperature and time on the failure characteristics of TIGA 321, EA913NA, EA946 (three filled epoxy adhesives). From the test data a 'Multi-Axial, Temperature, and Time Dependent' or MATT failure criterion was developed. It is shown that this criterion simplifies, for constant load and constant load rate conditions, into a form that can be easily used for stress analysis. Failure for TIGA 321 and EA9 13NA are characterized below their glass transition temperature. Failure for EA946 is characterized for conditions that pass through its glass transition. The MATT failure criterion is shown to be accurate for a wide range of conditions for these adhesives.