P.2. Poster Session on Propulsion Systems II

Papers

1. Influence of two air inlets on combustion efficiency of fuel-rich flow field laden with boron particle

2. Particle collection and influence of aggregation condition on particles size distribution of solid rocket motor

3. Numerical study on 3-d two-phase flow field for tail-pipe nozzle srm under high acceleration

4. Ablation model of thermal insulator in oxygen-rich condition

5. Experimental research on the low vulnerability of HTPB and NEPE solid propellant