Performance of a supersonic ramp-type side inlet with ram-scoop throat bleed and varying fuselage boundary-layer removal : Mach number range 1.5 to 2.0
| Author: | Mitchell, Glenn A. |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E56I26 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62848/ |