Analysis of longitudinal stability and trim of the Bell X-1 airplane at a lift coefficient of 0.3 to Mach numbers near 1.05
| Author: | Drake, Hubert M. |
|---|---|
| Additional Authors: | Carden, John R. |
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51H01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58887/ |