Longitudinal Stability and Drag Characteristics at Mach Numbers From 0.75 to 1.5 of an Airplane Configuration Having a 60 Degree Swept Wing of Aspect Ratio 2.24 as Obtained From Rocket-Propelled Models
| Author: | Vitale, A. James |
|---|---|
| Additional Authors: | McFall, John C., Jr. |
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51K06 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59274/ |
