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/metadc52850/ |