Buckling of Imperfect Anisotropic Circular Cylinders under Combined Loading
- 1 March 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 17 (3), 278-287
- https://doi.org/10.2514/3.61113
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Effect of prebuckling deformations on buckling of laminated composite circular cylindrical shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Buckling of imperfect anisotropic circular cylinders under combined loadingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Buckling and Vibration of Cross-Ply Laminated Circular Cylindrical ShellsAIAA Journal, 1975
- Buckling of laminated composite cylinders: a reviewComposites, 1975
- Combined compression-torsion buckling tests of laminated composite cylindrical shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Buckling of Laminated Anisotropic Imperfect Circular Cylinders under Axial CompressionJournal of Spacecraft and Rockets, 1973
- Buckling and postbuckling behavior of composite cylindrical shells under axial compressionAIAA Journal, 1970
- Buckling of Composite and Homogeneous Isotropic Cylindrical Shells Under Axial and Radial LoadingJournal of Applied Mechanics, 1969
- SOME PROBLEMS IN STABILITY OF HETEROGENEOUS AEOLOTROPIC CYLINDRICAL SHELLS UNDER COMBINED LOADINGAIAA Journal, 1963
- STABILITY OF HETEROGENEOUS AEOLOTROPIC CYLINDRICAL SHELLS UNDER COMBINED LOADINGAIAA Journal, 1963