Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8
| Author: | Schult, Eugene D |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57J28 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63951/ |