Modeling-driven damage tolerant design of graphene nonplatelet/carbon fiber/epoxy hybrid composite panels for full-scale aerospace structures

Authors

Julie Tomasi, Michigan Technological UniversityFollow
William Pisani, Michigan Technological University
Sorayot Chinkanjanarot, Michigan Technological UniversityFollow
Aaron Krieg, Michigan Technological UniversityFollow
John Jaszczak, Michigan Technological UniversityFollow
Julia A. King, Michigan Technological UniversityFollow
Ibrahim Miskioglu, Michigan Technological UniversityFollow
Gregory M. Odegard, Michigan Technological UniversityFollow
et. al.

Document Type

Conference Proceeding

Publication Date

1-6-2019

Department

Department of Mechanical Engineering-Engineering Mechanics; Department of Physics

Publisher's Statement

Publisher's version of record: https://doi.org/10.2514/6.2019-1273

Publication Title

AIAA Scitech 2019 Forum

Recommended Citation

Tomasi, J., Pisani, W., Chinkanjanarot, S., Krieg, A., Jaszczak, J., King, J. A., Miskioglu, I., Odegard, G. M., & et. al. (2019). Modeling-driven damage tolerant design of graphene nonplatelet/carbon fiber/epoxy hybrid composite panels for full-scale aerospace structures. AIAA Scitech 2019 Forum, 1273. http://doi.org/10.2514/6.2019-1273
Retrieved from: https://digitalcommons.mtu.edu/michigantech-p/279