2 pages matching turbine-discharge temperature in this book
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100 percent corrected 18 20 Corrected 20 Corrected inlet 78 Type Baseline compressor bleed doors circumferential distortion compressor discharge compressor face compressor maps compressor pressure ratio compressor stall compressor was mapped corrected airflow Corrected engine speed Corrected inlet airflow Distortion Baseline fig EFFECT OF SLOTTED effect of tip eight stages exhaust nozzle Extrapolated stall points Figure four inlet conditions Grooved hub radial distortion hub-radial distortion inlet airflow rate inlet configurations inlet distortion J85-13 compressor kg/sec Lewis Research Center MULTISTAGE COMPRESSOR NASA TM normal operating range Overall compressor efficiency percent corrected engine percent of rated Performance maps performance with slotted performance with untreated points Corrected engine pumping capacity rings in stages SLOTTED CASING TREATMENT stage stator stall margin stall points Corrected stall pressure ratio stall sites static pressure tip radial distortion tip-radial distortion tip-treatment total pressure TREATMENT ON PERFORMANCE turbine-discharge temperature Turbojet Type of data uniform inlet flow untreated rings wall treatment