Damage Propagation in Ductile Metals Subjected To Hypervelocity Impacts

901840

09/01/1990

Event
Aerospace Technology Conference and Exposition
Authors Abstract
Content
Hypervelocity impact damage on pressurized aluminum alloy tanks, due to orbital debris, was studied. The induced damaged area, as the results of the fragmented particles, was measured. The calculated damaged size was incorporated in the FMDM (fracture mechanics of ductile metals) model to predict catastrophic failure. The variation of the failure stress as a function of critical damaged size was plotted and was called damaged or failure curve. The failure predicted by the model collaborated with the experimental test results performed on several plates. These plates were subjected to biaxial loading simulated state of stress induced in the cylindrical pressurized tank.
Meta TagsDetails
DOI
https://doi.org/10.4271/901840
Pages
7
Citation
Farahmand, B., "Damage Propagation in Ductile Metals Subjected To Hypervelocity Impacts," SAE Technical Paper 901840, 1990, https://doi.org/10.4271/901840.
Additional Details
Publisher
Published
Sep 1, 1990
Product Code
901840
Content Type
Technical Paper
Language
English