The mass and stiffness distributions for helicopter rotor blades are tailored in such a way to give a predetermined placement of blade natural frequencies. The optimal design is pursued with respect of minimum weight, sufficient inertia, and reasonable dynamic characteristics. Finite element techniques are used as a tool. Rotor types include hingeless, articulated, and teetering.
Design of Helicopter Rotor Blades for Optimum Dynamic Characteristics
1985
116 pages
Report
Keine Angabe
Englisch
Optimum design of helicopter rotor blades with multidisciplinary couplings
Tema Archiv | 1992
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