Experiments and analysis for composite blades under large deflections. I - Static behavior
- 1 September 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (9) , 1573-1579
- https://doi.org/10.2514/3.25255
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Finite Element Approach to Rotor Blade ModelingJournal of the American Helicopter Society, 1987
- Aeroelastic Stability Analysis of a Composite Rotor BladeJournal of the American Helicopter Society, 1985
- The Nonlinear Behavior of Elastic Slender Straight Beams Undergoing Small Strains and Moderate RotationsJournal of Applied Mechanics, 1979
- Recent Developments in Rotary-wing AeroelasticityJournal of Aircraft, 1977