Damping in a roll of a missile configuration with a modified triangular wing and a cruciform tail at a Mach number of 1.52
| Author: | Scherrer, Richard |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A51A03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58739/ |