A parametric aircraft fuselage model for preliminary sizing and crashworthiness applications
Crossref DOI link: https://doi.org/10.1007/s13272-016-0193-4
Published Online: 2016-05-07
Published Print: 2016-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Schwinn, D. B.
Kohlgrüber, D.
Scherer, J.
Siemann, M. H.
Funding for this research was provided by:
Bundesministerium fur Wirtschaft und Technologie (DE) (20W0903C)
European Commission (BE) (FP7-266172)
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