Numerical Simulation of the Load Carrying Capability of Composite Rotorcraft Airframe Structures, Taking into Account the Effect of Disbonds in the Damage Tolerance and Fatigue Evaluation

Research output: Contribution to book/Conference proceedings/Anthology/ReportConference contributionContributedpeer-review

Contributors

Details

Original languageUndefined
Title of host publication72nd American Helicopter Society Annual Forum
Place of PublicationWest Palm Beach USA
Publication statusPublished - 2016
Peer-reviewedYes

External IDs

ORCID /0000-0003-1185-0046/work/155816261