Component tests to determine the aerodynamic characteristics of an all-moveable 70 degree delta canard-type control in the presence of a body at a Mach number of 1.61
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53I03 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59873/ |