The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength

Research output: Contribution to conferencePaper

Original languageEnglish
Publication statusPublished - 2016
Event5th Aircraft Structural Design Conference - Manchester, United Kingdom
Duration: 04 Oct 201606 Oct 2016

Conference

Conference5th Aircraft Structural Design Conference
CountryUnited Kingdom
CityManchester
Period04/10/201606/10/2016

Cite this

Harley, C., Quinn, D., Robinson, T., & Goel, S. (2016). The Effect of Panel Boundary Conditions on Laminate Damage Tolerant Strength. Paper presented at 5th Aircraft Structural Design Conference, Manchester, United Kingdom.