An investigation was conducted to determine the effects of water injection on the over-all performance of a modified J33-A-27 turbojet-engine compressor at the design equivalent speed of 11,800 rpm. The water-air ratio by weight was 0.05. With water injection the peak pressure ratio increased 9.0 per- cent, the maximum efficiency decreased 15 percent (actual numerical difference 0.12), and. the maximum total weight flow increased 9.3 percent.
Performance of J33-A-27 Turbojet-Engine Compressor
1950-01-01
Miscellaneous
No indication
English
Performance of J33-A-27 Turbojet-Engine Compressor
NTRS | 1949
|Performance of J33-A-23 Turbojet-Engine Compressor
NTRS | 1948
|Performance of J33-A-27 Turbojet-Engine Compressor
NTRS | 1950
|Performance of Compressor of XJ-41-V Turbojet Engine
NTRS | 1947
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