The subsonic static aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3. I : effects of horizontal-tail location and size on the longitudinal characteristics
| Author: | Tinling, Bruce E. |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-4041 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56477/ |