Performance of a Mach 3.0 External-Internal- Compression Axisymmetric Inlet at Mach Numbers from 2.0 to 3.5
1960
21 pages
Report
No indication
English
Axisymmetry , Internal compression inlet , Supersonic speed , Aerodynamics , Air , Annulus , Characteristics , Compression , Diffuser , External , Flow , Inlet , Internal , Nozzle , Performance , Speed , Subsonic , Supersonic