Flutter of flat, rectangular, orthotropic panels.
- 1 January 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (1) , 116-124
- https://doi.org/10.2514/3.3917
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- THE ROLE OF BOUNDARY CONDITIONS ON FLUTTER OF ORTHOTROPIC PANELSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- An application of the quadratic penalty function criterion to the determination of a linear control for a flexible vehicleAIAA Journal, 1965
- Effect of aerodynamic damping on flutter of thin panelsAIAA Journal, 1964
- Flutter of Thin Plates under Combined Shear and Normal Edge ForcesAIAA Journal, 1963
- On the Aeroelastic Stability of Orthotropic Panels in Supersonic FlowJournal of the Aerospace Sciences, 1962
- An Introduction to Applied Anisotropic ElasticityPhysics Today, 1961
- Vibration Characteristics of Stiffened PlatesJournal of Mechanical Engineering Science, 1960
- The Vibration of Rectangular PlatesProceedings of the Institution of Mechanical Engineers, 1954