Design and sizing of an aeroelastic composite model for a flying wing configuration with maneuver, gust, and landing loads
Crossref DOI link: https://doi.org/10.1007/s13272-020-00446-x
Published Online: 2020-04-11
Published Print: 2020-09
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Bramsiepe, Kjell
Voß, Arne
Klimmek, Thomas
Text and Data Mining valid from 2020-04-11
Version of Record valid from 2020-04-11
Article History
Received: 22 February 2018
Revised: 25 October 2019
Accepted: 6 March 2020
First Online: 11 April 2020