Lateral Stability Characteristics Between Mach Numbers of 0.80 and 1.57 and Simulation of Coupled Motion at Mach Number of 1.30 of a Rocket-Propelled Model of an Airplane Configuration Having Thin Highly Tapered 45 Degree Sweptback Surfaces
| Author: | D'Aiutolo, Charles T. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56A17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64361/ |