Investigation at Mach numbers 1.5 and 1.7 of twin-duct side intake system with two-dimensional 6 degree compression ramps mounted on a supersonic airplane
| Author: | Davids, Joseph |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E53H19 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59677/ |