Wind-Tunnel Tests of a Model of a Wingless Fin-Controlled Missile to Obtain Static Stability and Control Characteristics Through a Range of Mach Numbers From 0.5 to 0.88
| Author: | Burrows, Dale L. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53J06 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62754/ |