Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54B11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60170/ |