The Effects of the Addition of Small Fuselage-Mounted Fins on the Static Directional Stability Characteristics of a Model of a 45 Degree Swept-Wing Airplane at Angles of Attack up to 15.3 degrees at a Mach Number of 2.01
| Author: | Spearman, M. Leroy |
|---|---|
| Additional Authors: | Robinson, Ross B. |
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56D16a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62788/ |