Investigation of Effect of Sideslip on Lateral Stability Characteristics 2: Rectangular Midwing on Circular Fuselage With Variations in Vertical-Tail Area and Fuselage Length With and Without Horizontal Tail Surface
| Author: | Hollingworth, Thomas A. |
|---|---|
| Year: | 1945 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-8, NACA-ARR-L5C13 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60981/ |