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100 percent corrected 18 20 Corrected 20 Corrected inlet 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 grooves guide vanes hub radial distortion hub-radial distortion inlet airflow rate inlet configurations inlet distortion inlet temperature J85-13 compressor kg/sec Lewis Research Center line 80 located MULTISTAGE COMPRESSOR N/cm normal operating range Overall compressor efficiency percent corrected engine percent of rated Performance maps performance with slotted performance with untreated points Corrected engine presents the effect pumping capacity rated 80 rated speed rings in stages stage stator stall margin stall points Corrected stall pressure ratio stall sites tip radial distortion tip-radial distortion tip-treatment total temperature turbine-discharge temperature Type of data uniform inlet flow untreated rings