Investigation of the Effects of Wing and Tail Modifications on the Low-Speed Stability Characteristics of a Model Having a Thin 40 Degree Swept Wing of Aspect Ratio 3.5
| Author: | Weil, Joseph |
|---|---|
| Additional Authors: | Sleeman, William C., Jr. |
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53C09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59733/ |