L. Librescu et al., VIBRATION OF GEOMETRICALLY IMPERFECT PANELS SUBJECTED TO THERMAL AND MECHANICAL LOADS, Journal of spacecraft and rockets, 33(2), 1996, pp. 285-291
The results of a study of the vibration response of transversely isotr
opic flat and curved panels subjected to temperature fields and to mec
hanical loads into the postbuckling load range are presented, The resu
lts were obtained using a higher-order transverse-shear-deformation th
eory of shallow shells that includes the effects of geometric nonlinea
rities and initial geometric imperfections, The results focus on the i
nteraction between the temperature field, the applied mechanical load,
and the fundamental frequency associated with small vibrations about
the prebuckling and postbuckling equilibrium states. Results are prese
nted for a wide range of temperatures and mechanical load magnitudes a
nd of geometric parameters. The results show that transverse-shear fle
xibility has a significant effect on the analytical prediction of pane
l response and that the fundamental frequency of a panel may be substa
ntially overestimated in the prebuckling load range and underestimated
in the postbuckling load range, Results are also presented that indic
ate that the fundamental frequency of flat panels generally increases
as the initial geometric imperfection amplitude increases for both the
prebuckling and postbuckling load ranges, The results, however, also
indicate that the fundamental frequency of curved panels generally dec
reases in the prebuckling load range and increases in the postbuckling
load ranges.