Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics 5: Symmetrically Tapered Wing With a Circular Fuselage Having a Horizontal and a Vertical Tail
| Author: | Wallace, Arthur R. |
|---|---|
| Year: | 1943 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-459, NACA-ARR-3F23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61017/ |