Abstract The basic equations of the main rotor blade motion with the preservation of nonlinear terms are presented. The results of analyzing the term values for nonlinear equations obtained for different flight regimes and several aeroelasticity problems are given.
Study of feasibility and exactness for the mathematical “semirigid” nonlinear model of the helicopter main rotor
Russian Aeronautics (Iz VUZ) ; 55 , 4 ; 357-365
2012-10-01
9 pages
Article (Journal)
Electronic Resource
English