Reliability-based aeroelastic design of composite plate wings using a stability margin
Crossref DOI link: https://doi.org/10.1007/s00158-017-1838-6
Published Online: 2017-11-20
Published Print: 2018-04
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Scarth, Carl http://orcid.org/0000-0002-7184-9808
Cooper, Jonathan E.
Funding for this research was provided by:
Engineering and Physical Sciences Research Council (EP/G036772/1)
Embraer S.A.
University of Bristol
License valid from 2017-11-20