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Computational Research of the Main Rotor Steep Descent Modes Based on the Nonlinear Blade Vortex Model

Crossref DOI link: https://doi.org/10.3103/S1068799819020107

Published Online: 2019-09-09

Published Print: 2019-04

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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