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TECHNICAL PAPERS

Effects of In-plane Load on Flutter of Homogeneous Laminated Beam Plates with Delamination

[+] Author and Article Information
Le-Chung Shiau, Yuan-Shih Chen

  National Cheng Kung University, Tainan, Taiwan 70101, ROC

J. Vib. Acoust 123(1), 61-66 (Jul 01, 2000) (6 pages) doi:10.1115/1.1315593 History: Received September 01, 1999; Revised July 01, 2000
Copyright © 2001 by ASME
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References

Dowell,  E. H., 1964, “Flutter of Multibay Panels at High Supersonic Speeds,” AIAA J., 2, No. 10, pp. 1805–1814.
Dugundji,  J., 1966, “Theoretical Consideration of Panel Flutter at High Supersonic Mach Numbers,” AIAA J., 4, No. 7, pp. 1257–1266.
Fung,  Y. C., 1963, “Some Recent Contributions to Panel Flutter Research,” AIAA J., 1, No. 11, pp. 898–909.
Kariappa,  , Fung,  Y. C., Somashekar,  B. R., and Shah,  C. G., 1970, “Discrete Element Approach to Flutter of Skew Panels with In-Plane Forces under Yawed Supersonic Flow,” AIAA J., 8, No. 11, pp. 2017–2022.
Olson,  M. D., 1970, “Some Flutter Solutions Using Finite Elements,” AIAA J., 8, No. 4, pp. 747–752.
Sander,  G., Bon,  C., and Geradin,  M., 1973, “Finite Element Analysis of Supersonic Panel Flutter,” Int. J. Numer. Methods Eng., 7, 379–394.
Calligeros,  J. M., and Dugundji,  J., 1963, “Effects of Orthotropicity Orientation on Supersonic Panel Flutter,” AIAA J., 1, No. 9, pp. 2180–2182.
Ketter,  D. J., 1967, “Flutter of Flat Rectangular Orthotropic Panels,” AIAA J., 5, No. 1, pp. 116–124.
Liaw,  D. G., 1993, “Supersonic Flutter of Laminated Thin Plates with Thermal Effects,” AIAA J., 30, No. 1, pp. 105–111.
Ramkumar,  R. L., and Weisshaar,  T. A., 1977, “Flutter of Flat Rectangular Anisotropic Plates in High Mach Number Supersonic Flow,” J. Sound Vib., 50, No. 4, pp. 587–597.
Rossettos,  J. N., and Tong,  P., 1974, “Finite-Element Analysis of Vibration and Flutter of Cantilever Anisotropic Plates,” ASME J. Appl. Mech., 41, No. 4, pp. 1075–1080.
Sawyer,  J. W., 1977, “Flutter and Buckling of General Laminated Plates,” J. Aircr., 14, No. 4, pp. 387–393.
Shiau,  L. C., and Chang,  J. T., 1990, “Transverse Shear Effect on Flutter of Composite Panels,” ASCE, J. Aerosp. Eng.,5, No. 4, pp. 465–479.
Shiau,  L. C., and Chang,  J. T., 1991, “Finite Element Analysis of Supersonic Flutter of Multibay Composite Panels,” J. Comput. Struct. 39, No. 3/4, pp. 269–276.
Shiau,  L. C., 1992, “Flutter of Composite Laminated Beam Plates with Delamination,” AIAA J., 30, No. 10, pp. 2504–2511.
Shiau,  L. C., 1993, “Delamination Effect on Flutter of Homogeneous Laminated Plates,” ASCE J. Aerosp. Eng., 6, No. 3, pp. 284–298.
Simitses,  G. J. , 1985, “Effect of Delamination of Axially Loaded Homogeneous Laminated Plates,” AIAA J., 23, No. 9, pp. 1437–1444.
Tracy,  J. J., and Pardoen,  G. C., 1989, “Effects of Delamination on the Natural Frequencies of Composite Laminates,” J. Compos. Mater., 23, 1200–1215.
Yin,  W. L., , 1986, “Ultimate Axial Load Capacity of a Delaminated Beam-plate,” AIAA J., 24, No. 1, pp. 123–128.

Figures

Grahic Jump Location
Flutter boundary vs in-plane force (d=0.5,h2/h=0.5)
Grahic Jump Location
Flutter boundary vs delamination length (h2/h=0.5)
Grahic Jump Location
Flutter boundary vs delamination location (h2/h=0.5)
Grahic Jump Location
Flutter boundary vs delamination length (h2/h=0.25)
Grahic Jump Location
Flutter boundary vs delamination location (h2/h=0.25)
Grahic Jump Location
Flutter boundary vs in-plane force (c=0.3,h2/h=0.5)
Grahic Jump Location
Dynamic pressure vs eigenvalue (d=0.5,c=0.34,h2/h=0.5)

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