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Nine-Node Resultant-Stress Shell Element for Free Vibration and Large Deflection of Composite Laminates.

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  • المؤلفون: Han, S. C.1; Choi, S.2 ; Chang, S. Y.3
  • المصدر:
    Journal of Aerospace Engineering. Apr2006, Vol. 19 Issue 2, p103-120. 18p. 15 Diagrams, 5 Charts, 5 Graphs.