Rate Dependent Strength Characterization of Carbon Fiber Composite Laminates
| dc.contributor.advisor | Waas, Anthony | |
| dc.contributor.author | Marek, Jaspar | |
| dc.date.accessioned | 2017-08-11T22:48:42Z | |
| dc.date.available | 2017-08-11T22:48:42Z | |
| dc.date.issued | 2017-08-11 | |
| dc.date.submitted | 2017-06 | |
| dc.description | Thesis (Master's)--University of Washington, 2017-06 | |
| dc.description.abstract | The implementation of carbon fiber laminates in commercial vehicles is becoming increasingly common. Characterization of these materials for modeling is often completed at quasi-static loading rates regardless of the loading rates the final part will experience. This thesis will discuss the rate dependency of strength characteristics and Schapery parameters of a composite laminate under quasi-static, intermediate, and high rate loading conditions. | |
| dc.embargo.terms | Open Access | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.other | Marek_washington_0250O_17440.pdf | |
| dc.identifier.uri | http://hdl.handle.net/1773/39926 | |
| dc.language.iso | en_US | |
| dc.rights | none | |
| dc.subject | Carbon Fiber | |
| dc.subject | Composite Laminates | |
| dc.subject | Open Hole Tension | |
| dc.subject | Rate Dependent | |
| dc.subject | Schapery Theory | |
| dc.subject | Split Hopkinson Bar | |
| dc.subject | Aerospace engineering | |
| dc.subject.other | Aeronautics and astronautics | |
| dc.title | Rate Dependent Strength Characterization of Carbon Fiber Composite Laminates | |
| dc.type | Thesis |
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