Influence of Wing and Fuselage on the Vertical-Tail Contribution to the Low-Speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces
| Author: | Wolhart, Walter D. |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2587 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56208/ |