Abstract
A numerical study was conducted to investigate the effect of porosity strength on the drag reduction of a transonic projectile having the secant-ogival-cylindrical boat-tail shape (SOBCT)
| Original language | English |
|---|---|
| Pages (from-to) | 310-316 |
| Number of pages | 7 |
| Journal | Journal of Aircraft |
| Volume | 44 |
| Publication status | Published - Jan 2007 |