Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7
| Author: | Chubb, Robert S |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52G29 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59344/ |