Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5
| Author: | Lampkin, Bedford A. |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A58F17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64332/ |