Formulation of the aeroelastic stability and response problem of coupled rotor/support systems
- 4 April 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Recent Developments in Rotary-wing AeroelasticityJournal of Aircraft, 1977
- The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller‐RotorsJournal of the American Helicopter Society, 1967
- Prop‐Rotor Stability at High Advance RatiosJournal of the American Helicopter Society, 1966
- Mechanical Stability of a Two-Bladed Cantilever Helicopter RotorJournal of the Aeronautical Sciences, 1956