Aeroelastic response and blade loads of a composite rotor in forwardflight
- 13 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 26 references indexed in Scilit:
- Formulation and Evaluation of an Analytical Model for Composite Box‐BeamsJournal of the American Helicopter Society, 1991
- Rotor Loads Prediction Utilizing a Coupled Aeroelastic Analysis with Refined Aerodynamic ModelingJournal of the American Helicopter Society, 1991
- Experiments and analysis for composite blades under large deflections. II - Dynamic behaviorAIAA Journal, 1990
- Experiments and analysis for composite blades under large deflections. I - Static behaviorAIAA Journal, 1990
- Review of composite rotor blade modelingAIAA Journal, 1990
- Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approachAIAA Journal, 1989
- Validation of approximate indicial aerodynamic functions for two-dimensional subsonic flowJournal of Aircraft, 1988
- Finite Element Analysis for Bearingless Rotor Blade AeroelasticityJournal of the American Helicopter Society, 1984
- On a hierarchy of conforming timoshenko beam elementsComputers & Structures, 1981
- The effects of fibre orientation on free vibrations of composite beamsJournal of Sound and Vibration, 1980