Aeroelastic Modeling of Swept Tip Rotor Blades Using Finite Elements
- 1 April 1988
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 33 (2) , 43-52
- https://doi.org/10.4050/jahs.33.43
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Technical Note: Assembly of Moderate‐Rotation Finite Elements Used in Helicopter Rotor DynamicsJournal of the American Helicopter Society, 1987
- Use of an implicit formulation based on quasilinearization for the aeroelastic response and stability of rotor blades in forward flightPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A general model of the dynamics of moving and rotating rodsComputers & Structures, 1985
- Coupled Flap‐Lag‐Torsional Dynamics of Hingeless Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1982
- Influence of Modeling and Blade Parameters on the Aeroelastic Stability of a Cantilevered RotorAIAA Journal, 1977