Lateral Stability Characteristics at Low Lift Between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback
| Author: | D'Aiutolo, Charles T. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55A31 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61131/ |