Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degree Sweptback Wing and Tail as Obtained by the Transonic-Bump Method
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L8C11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57556/ |