Modeling the Elastic and Damping Properties of the Multilayered Torsion Bar-Blade Structure of Rotors of Light Helicopters of the New Generation 2. Finite-Element Approximation of Blades and a Model of Coupling of the Torsion Bar with the Blades
Crossref DOI link: https://doi.org/10.1007/s11029-016-9548-5
Published Online: 2016-01-13
Published Print: 2016-01
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Paimushin, V. N.
Shishkin, V. M.
Text and Data Mining valid from 2016-01-01
