Free-flight experience of the lateral stability characteristics at low lift of a 45 degree swept-wing rocket-propelled model equipped with a nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73
| Author: | D'Aiutolo, Charles T. |
|---|---|
| Additional Authors: | Willoughby, William W. |
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56L18 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64183/ |