The reliability evaluation ways of all kinds of units in launching dynamical system is discussed in this paper.

Calculation of launch dynamics with two-phase flow interior ballistic model for self-propelled artillery;

Launch Dynamics of Tactical Missile and Simulation;

Based on launch dynamics,multibody system transfer matrix method and ballistic theory,simulation code was written by using Monte Carlo method.

According to the up-to-date theories from the launching dynamics and the multi-body system dynamics and utilizing the established simulation system which can precisely depict the motion law of the long range MLRS,The relationship of the shot accuracy between short,middle and maximum range can be quantitatively defined,so an it can be used to realize the reduced computation of different range.

Based on the dynamics equation of shipboard gun component, by using the numerical integral method and expanding the transfer matrix method of vibration mechanics, this paper established a blocking method for launching dynamics of shipboard gun, which was named the discrete time transfer matrix method for launching dynamics of shipboard gun.

Aim To present an analytical method for the launching dynamics of self propelled cannons and to illustrate its feasibility by comparing the analytical and simulation results with the related on spot test results.

The flow parameters which describe directe flow, squeezeout and elliptic flow, as well as probing the equation of state, in medium nn cross section and the dynamical emission are reviewed.