Development of the discrete vortex cylinders method for calculating the helicopter rotor induced velocity
Crossref DOI link: https://doi.org/10.3103/S1068799816010025
Published Online: 2016-07-06
Published Print: 2016-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Nikolaev, E. I.
Nikolaeva, M. N.
License valid from 2016-01-01