A method for predicting the performance of high reaction supersonic compressor blade sections.
Supersonic compressor blade sections performance prediction near maximum pressure ratio and efficiency by analyzing flow processes
Boxer, E.↗
Engineering topics
Boxer, E.
Publications and source records attributed to Boxer, E..
The variable-pitch supersonic inflow compressor and its application in a hypersonic engine
Explore the source record for details and available documents.
Boxer, E.↗
The flow induction process of compressors designed to accept supersonic inflow velocity.
Supersonic compressor flow induction process as affected by Mach number, cone angle, rotational speed and blade angle
MACH NUMBER↗