Vibration tailoring of advanced composite lifting surfaces
- 1 February 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (2) , 141-147
- https://doi.org/10.2514/3.45098
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Frequency determination and non-dimensionalization for composite cantilever platesJournal of Sound and Vibration, 1980
- The identification of low energy K and Ca + autoionizing levels observed in electron impact experimentsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1979
- Aeroelastic Stability and Performance Characteristics of Aircraft with Advanced Composite Sweptforward Wing StructuresPublished by Defense Technical Information Center (DTIC) ,1978
- The dynamic elastic behaviour of a fibre-reinforced composite sheet. I. The precise experimental determination of the principal elastic moduliJournal of Physics D: Applied Physics, 1975
- The dynamic elastic behaviour of a fibre-reinforced composite sheet. II. The transfer matrix calculation of the resonant frequencies and vibration shapesJournal of Physics D: Applied Physics, 1975
- Torsion-flexure coupling in a composite materialJournal of Physics D: Applied Physics, 1974
- The Vibration of Cantilever Beams of Fiber Reinforced MaterialJournal of Composite Materials, 1972
- Vibration Characteristics of Unidirectional Filamentary Composite Material PanelsPublished by ASTM International ,1972
- The significance of coupling between shear and extension in the elastic behaviour of wood and plywoodProceedings of the Physical Society, 1943
- Interpretation of Torsional Frequencies of Crystal SpecimensPhysical Review B, 1940