ANALYSIS OF THE DYNAMIC BEHAVIOR, BUCKLING, AND AEROELASTICITY OF A THIN COMPOSITE PLATE WITH THE EFFECT OF GENERAL AND LOCAL GEOMETRIC DEFECTS

Author:

Moosazadeh H.,Mohammadi M. M.

Publisher

Pleiades Publishing Ltd

Reference35 articles.

1. R. O. Stearman, M. H. Lock, and Y. C. Fung, “Ames Tests on the Flutter of Cylindrical Shells," GALCIT Structural Dynamics Report SM 62-37 (California Inst. of Technol., 1962).

2. E. H. Dowell, “Nonlinear Flutter of Curved Plate. Pt 1," AIAA J. 7 (3), 424–431 (1969).

3. E. H. Dowell, “Nonlinear Flutter of Curved Plate. Pt 2," AIAA J. 8 (2), 261–263 (1970).

4. W. J. Anderson, “Experiments on the Flutter of Flat and Slightly Curved Panels at Mach Number 2.81," GALCIT Structural Dynamics Report SM 62-34 (California Inst. of Technol., 1962).

5. J. W. Sawyer, “Flutter and Buckling of General Laminated Plates," J. Aircraft 14 (4), 38793 (1977).

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