The dynamic stability of a viscoelastic plate in a supersonic gas flow and
subjected to a stochastically fluctuating axial thrust is performed within
the concept of the Lyapunov exponent. The constitutive relation is modeled
in an integral form by using the Boltzmann superposition principle. The pis
ton theory as a quasi-first-order approximation is used to represent the ae
rodynamic loading on the plate. The stochastic averaging method is used and
the Khasminskii's technique [Khasminskii, R, A., "Necessary and Sufficient
Conditions for the Asymptotic Stability of Linear Stochastic System," Theo
ry of Probability. and Its Application, Vol. 12, No. 1, 1967, pp, 144-147 (
English translation)] is employed to obtain the stability boundaries. The i
nfluence of the various plate and flow parameters and the random loading sp
ectral densities on the stability are investigated.