The first shock reflection within truncated plug nozzle propulsive jets is investigated experimentally using a free jet blow-down facility. The locations and sizes of these reflections in axisymmetric plug nozzles, with cylindrical shrouds and conical truncated plugs, are presented. Data are presented for a range of ambient to nozzle total pressure ratios. The effects of Mach disk location and size resulting from changing plug length and from varying amounts of base bleed are documented.
The Mach disc in truncated plug nozzle flows
American Institute of Aeronautics and Astronautics, Fluid and Plasma Dynamics Conference ; 1975 ; Hartford, CT
1975-06-01
Conference paper
No indication
English
The Mach disc in truncated plug nozzle flows
AIAA | 1975
|Mach Disk In Truncated Plug Nozzle Flows
AIAA | 1976
|