Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52 (Listing Multiple Pages).
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930086518.pdf | 935.7 KB | application/pdf | Download |
| Filename | Size | Format | Download |
|---|---|---|---|
| 19930086518.pdf | 935.7 KB | application/pdf | Download |