Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined From Flight Test for a Mach Number Range of 1.1 to 1.8
| Author: | Lundstrom, Reginald R. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55L16 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53134/ |