Transonic aeroelasticity analysis for rotor blades
- 1 May 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 29 (3) , 477-484
- https://doi.org/10.2514/3.46186
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Blade Response Calculations Using Three‐Dimensional Aerodynamic ModelingJournal of the American Helicopter Society, 1991
- Euler solution of the transonic flow for a helicopter rotorPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Finite Element Analysis for Bearingless Rotor Blade AeroelasticityJournal of the American Helicopter Society, 1984
- Application of the Finite Element Method to Rotary‐Wing AeroelasticityJournal of the American Helicopter Society, 1980