Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28
| Author: | Savin, Raymond C. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A55K21 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62366/ |