Influences of particle size of HMX on detonation waves propagation of HMX and HMX/F_(2641);

Numerical simulation of standing oblique detonation wave using parallel computation method;

Numerical simulation of gaseous detonation waves propagation and comparison with experimental results;

Numerical investigation of detonation direct initiation induced by toroidal shock wave focusing;

Study on the detonation cellular structure of propylene epoxide-Air;

A numerical investigation on the performance of a backward-forward double-detonation driver for high enthalpy shock tubes was conducted by solving one-dimensional Euler equations with the Dispersion Controlled Dissipative (DCD) scheme.

This paper presents the experimental results of the initiation and stabilization of an oblique detonation by launching a hypervelocity projectiles at velocities of 1700～2100m/s,into H 2 air mixtures.

The oblique detonation stabilized on a hypervelocity projectile was researched by numerical simulations and experimental visualizations.

It is important to study the ignition,growth and propagation of the laser supported detonation waves.

In order to carry out an investigation for the influence of physical and geometricl boundary conditions on the propagation of gaseous detonation waves, a double walled detonation shock tube (40×40mm square section) on hand is reconstructed.

The results of experiment and theoretical analysis are show that the defects occurred in interface is related to the orientation of detonation waves propagating and the open position of gap pillars,and that the defects can be eliminated or reduced.