According to Hamilton principle,transient aeroelastic response model of rotor blade was derived based on generalized forces formulation including ship motions.

To investigate the influences of the motions of ship on shipboard helicopter rotor transient aeroelastic response,the moderate deflection beam model was adopted to deal with the elastic deflections of blade and finite rotations were used to simulate rigid rotations of blade about hinges and rotor axis.

The instantaneous response of a laminar diffusion flamelet is investigated numerically.

Then we use the modality analysis to get the instantaneous response of the system to the outside stimulation.

Analysis of transient responses in piezoelectric laminates excited by coupled electro-mechanical loads;

Transient response research of steel spring impacted by shoprt wave;

Behavior of transient response of MR damper;

Simulation on the dynamic response of PEMFC stack power output;

This paper presents a new solution of the large deflection dynamic response of stiffened plates under lateral impact loading.

The normal mode theory is used to provide transient dynamic responses for the equations of motion.

Numerical simulation of transient thermal response of barrel when naval gun firing;

By numerical simulation,transient thermal response of the spherical aerostat in rising process was presented.