In recent years the investigation of dynamical behavior of plates under the
rmal loads has become Important because of the high temperatures reached on
external skin panels of hypersonic vehicles. Other researchers have indica
ted that the skin panels may encounter chaotic vibrations about their therm
ally buckled positions. In this research the chaotic vibrations of simply s
upported plates under thermal and sinusoidal excitation is studied to deter
mine the predictability of the vibratory behavior of a representative class
of such skin panels. The boundaries of regular and chaotic regions of moti
on are defined In force temperature and force frequency planes and the sens
itivity of these boundaries to changes in design parameters is explored for
the purpose of developing useful design criteria. The onset of chaos is pr
edicted through the computation of Lyapunov exponents. The effects of therm
al moment and thermal buckling on chaos are studied. The results of the res
earch are presented as a contribution to the panel design of hypersonic veh
icles.