Integral system project design of missile propelled by unchoked solid rocket ramjet can bring the performance of the solid rocket ramjet and missile into play and make them work in harmony,and improve the performance of the missile and ramjet.

Quick-forecasting algorithm for performance of solid rocket ramjet;

Some technological problems of solid rocket ramjet;

Experimental study on solid rocket ramjet with central air-inlet mode;

There are a variety of influential factors to the combustion efficiency of secondary chamber of boron-based propellant ducted rocket motor,which are difficult to be expressed accurately by analytical functions.

Erosion test of the insulation in the ramjet combustor of solid ducted rocket motors;

The 3D reaction flow field in the afterburning chamber of solid ducted rocket motor with binary dual-underside inlet mode was numerically simulated by means of RNG κ-ε turbulence model and one step eddy-dissipation combustion model.

By direct-conncted simulation calculation,the effects of common heater fuel (hydrogen,kerosene,methane and alcohol) on performance of solid ducted rocket motor with low-oxygen boron-based propellant were investigated.

Modeling and simulation on the gas generator and gas control valve of solid ducted rockets;

Three dimension numerical simulation on air inlet of solid ducted rocket;

Dynamic modeling and model reduction order of controllable flow solid ducted rockets;