Performance Enhancement of a Composite Tilt-Rotor Using Aeroelastic Tailoring
- 1 September 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 37 (5), 850-858
- https://doi.org/10.2514/2.2680
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- VABS: A New Concept for Composite Rotor Blade Cross-Sectional ModelingJournal of the American Helicopter Society, 1997
- Cross-sectional analysis of composite beams including large initial twist and curvature effectsAIAA Journal, 1996
- Extension-twist behavior of initially twisted composite spars for tilt-rotor applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Aeroelastic optimization of a helicopter rotor with composite couplingJournal of Aircraft, 1995
- Decomposition-based optimization procedure for high-speed prop-rotors using composite tailoringJournal of Aircraft, 1995
- Demonstration of an elastically coupled twist control concept for tilt rotor blade applicationAIAA Journal, 1994
- Structural behavior of two-cell composite rotor blades with elastic couplingsAIAA Journal, 1992
- Approach for analysis and design of composite rotor bladesJournal of Aircraft, 1992
- Theory of anisotropic thin-walled closed-cross-section beamsComposites Engineering, 1992
- A mixed variational formulation based on exact intrinsic equations for dynamics of moving beamsInternational Journal of Solids and Structures, 1990