Abstract
Flight stability and rear flow fields of the cargo projectile were studied by simulation test and numerical computation. The cargo projectile can fly stably and the results of simulation test agree well with numerical computation. In addition, the rear pressure distribution was also obtained by numerical computation, showing that there are eddy-current zones at the bomb rear, which will increase with the flight speed.
| Original language | English |
|---|---|
| Pages (from-to) | 107-113 |
| Number of pages | 7 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 25 |
| Issue number | 1 |
| Publication status | Published - Jan 2010 |
Keywords
- Eddy-current zone
- Flight stability
- Rear flow fields
- Simulation test