Abstract
A numerical analysis was performed to study convective burning flow field in solid propellant crack. The implicit TVD scheme was used to solve the two-dimensional Navier-Stokes equation with gas injection and erosive burning. The pressure distribution inside the crack was obtained and the relation between the length and height of crack and the pressure in crack tip was also discussed.
| Original language | English |
|---|---|
| Pages (from-to) | 36-39 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 20 |
| Issue number | 3 |
| State | Published - 1999 |