Nonlinear aeroelastic stability analysis of hingeless helicopter rotor blades using FRF coupling and condition number
Work
Year: 2015
Type: article
Source: Nonlinear Dynamics
Cites: 15
Cited by: 1
Related to: 10
FWCI: 0.358
Citation percentile (by year/subfield): 48.06
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Sustainable Development Goal Affordable and clean energy
Open Access status: closed