An investigation of the lift, drag, and static-stability characteristics of a triangular-wing airplane configuration at Mach numbers from 3.00 to 6.28
| Author: | Gloria, Hermilo R |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A56H27 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62903/ |