Experimental-theoretical investigation of the vibration characteristics of rotating composite box beams
- 1 July 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 29 (4) , 657-664
- https://doi.org/10.2514/3.46216
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Thin-walled composite beams under bending, torsional, and extensional loadsJournal of Aircraft, 1990
- Nonclassical Behavior of Thin‐Walled Composite Beams with Closed Cross SectionsJournal of the American Helicopter Society, 1990
- Formulation and Evaluation of An Analytical Model for Composite Box-BeamsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Structural Dynamics of a Helicopter Rotor Blade SystemJournal of the American Helicopter Society, 1990
- Finite-Element Model for Composite Beams with Arbitrary Cross-Sectional WarpingAIAA Journal, 1988
- Use of piezoelectric actuators as elements of intelligent structuresAIAA Journal, 1987
- Extension-twist coupling of composite circular tubes with application to tilt rotor blade designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Aeroelastic Stability Analysis of a Composite Bearingless Rotor BladeJournal of the American Helicopter Society, 1986
- Aeroelastic Stability Analysis of a Composite Bearingless Rotor BladeJournal of the American Helicopter Society, 1986
- Aeroelastic Stability Analysis of a Composite Rotor BladeJournal of the American Helicopter Society, 1985