Wind Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics: [Part] 4 - Symmetrically Tapered Wing With a Circular Fuselage Having a Wedge-Shaped Rear and a Vertical Tail
| Author: | Recant, I. G. |
|---|---|
| Year: | 1942 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-520, NACA-ARR |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61016/ |