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46                 Polymer-based Nanocomposites for Energy and Environmental Applications


          Table 2.6 Experimental data of sandwich composites [37]
          Type of core    No. of specimen  Maximum load (N)    Average load (N)

          Neat polycore   1                 730                 700
                          2                 596
                          3                 774
                          1                1170                1073
          TiO 2
                          2                1047
                          3                1003

         beams and the natural frequencies of sandwich beams are affected directly by the face
         materials; decrease by increasing the fiber orientations of the graphite/epoxy face lam-
         inates and increasing the thickness of the cores increases both the natural frequencies
         and the loss factors of the sandwich beams. Because of a better cross-linking, the phe-
         nolic resin has a loss factor greater than that of epoxy resin. The experimental results
         agree satisfactorily with those from finite element analysis. Fig. 2.19 shows the natural
         frequencies of sandwich beams for varied cases from experiment and finite element
         analysis.
            Hosur et al. [39] have fabricated the sandwich panels with neat and nanophased
         foam cores and three-layered plain weave carbon fabric/SC-15 epoxy-nanoclay com-
         posite face sheets. Sandwich panels are fabricated with different types of core and face



                5000                                     Experiment
                                                              [0] 4 /4mm core
                                                              [0] 4
                4000                                          [+30/–30] S S
                                                              [+45/–45]
               Natural frequency (Hz)  3000              FEM  [90] 4 /4mm core
                                                              [+60/–60]
                                                                    S


                                                              [0] 4
                2000
                                                              [0]
                                                               4
                                                              [+45/–45]
                1000                                          [+30/–30] S S
                                                              [+60/–60] S
                                                              [90] 4
                   0
                        1             2              3
                                      Mode number
         Fig. 2.19 Natural frequencies of sandwich beams from experiment and finite element
         analysis [38].
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