Technical Note: Assembly of Moderate‐Rotation Finite Elements Used in Helicopter Rotor Dynamics
- 1 October 1987
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 32 (4) , 63-69
- https://doi.org/10.4050/jahs.32.63
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Aeroelastic Modeling of Swept Tip Rotor Blades Using Finite ElementsJournal of the American Helicopter Society, 1988
- Introduction to GRASP—General Rotorcraft Aeromechanical Stability Program—A Modern Approach to Rotorcraft ModelingJournal of the American Helicopter Society, 1987
- Dynamic Stability of a Rotor Blade Using Finite Element AnalysisAIAA Journal, 1982
- Application of the Finite Element Method to Rotary‐Wing AeroelasticityJournal of the American Helicopter Society, 1980
- Technical Notes: The Effects of Second Order Blade Bending on the Angle of Attack of Hingeless Rotor BladesJournal of the American Helicopter Society, 1973