The Longitudinal Stability and Control Characteristics of a 60 Degree Delta-Wing Missile Having Half-Delta Tip Controls as Obtained From a Free-Flight Investigation at Transonic and Supersonic Speeds
| Author: | Moul, Martin T. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L52H14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59413/ |