High-Fidelity Aero-Structure Gradient Computation Techniques. Application to the Onera M6 Wing
Crossref DOI link: https://doi.org/10.1007/978-3-319-67988-4_37
Published Online: 2017-12-06
Published Print: 2018
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Achard, Timothée
Blondeau, Christophe
Ohayon, Roger
License valid from 2017-12-06