Numerical investigation of the vortex roll-up from a helicopter blade tip using a novel fixed-wing adaptation method
Crossref DOI link: https://doi.org/10.1007/s13272-016-0234-z
Published Online: 2017-01-07
Published Print: 2017-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Joulain, Antoine
Desvigne, Damien
Alfano, David
Leweke, Thomas
License valid from 2017-01-07