Use of an implicit formulation based on quasilinearization for the aeroelastic response and stability of rotor blades in forward flight
- 6 April 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Gust Response of Hingeless RotorsJournal of the American Helicopter Society, 1986
- Aeroelastic Stability Analysis of a Composite Rotor BladeJournal of the American Helicopter Society, 1985
- Flap-lag damping of an elastic rotor blade with torsion and dynamic inflow in hover from symbolically generated equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Aeroelastic stability of an elastic circulation control rotor blade in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1982
- Dynamic Stability of a Rotor Blade Using Finite Element AnalysisAIAA Journal, 1982
- Failure Indication and Corrective Action for Turboshaft EnginesJournal of the American Helicopter Society, 1980
- Application of the Finite Element Method to Rotary‐Wing AeroelasticityJournal of the American Helicopter Society, 1980