Experimental Investigation at High Subsonic Speeds to Determine the Rolling-Stability Derivatives of Three Wing-Fuselage Configurations
| Author: | Sleeman, William C., Jr. |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54H11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60656/ |