Wind-Tunnel Investigation at a Mach Number of 2.01 of the Aerodynamic Characteristics in Combined Pitch and Sideslip of Some Canard-Type Missiles Having Cruciform Wings and Canard Surfaces With 70 Degree Delta Plan Forms
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54F09 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60415/ |