AEATECHNOLoGY ENGINEERING SOFTWAR Case stud >PROGRAM CON TROL MAXIMUM NUMBER OF ITERATIONS 200 OUTPUT MONITOR POSITIoN 0.1070.04760.0275 MASS SOURCE TOLERANCE 1.0000E-06 >>MODEL BOUNDARY CONDITIONS >>INLET BOUNDARIES PATCH NAME INLET1 NORMAL VELOCITY 4.0000E-01 * W VELOCITY 4.0000E-01 K3.2000E-04 EPSILON 1.5260E-05 TEMPERATURE 3.0500E+02 >>工 NLET BOUNDARIES PATCH NAME INLET2 NORMAL VELOCITY 6.0000E-01 * W VELOCITY -6.0000E-01 K7.2000E-04 EPSILON 5.1520E-05 TEMPERATURE 2.9500E+02 >>WALL BOUNDARIES PATCH NAME WALL1 CFX-4.3V4.3.1H TEMPERATURE 2.8800E+02 CFX-4 Introductory Training (Dec 1999)CFX-4 Introductory Training (Dec 1999) 7-6 CFX-4.3 V4.3.1H Case Study >>SOLVER DATA >>PROGRAM CONTROL MAXIMUM NUMBER OF ITERATIONS 200 OUTPUT MONITOR POSITION 0.107 0.0476 0.0275 MASS SOURCE TOLERANCE 1.0000E-06 >>MODEL BOUNDARY CONDITIONS >>INLET BOUNDARIES PATCH NAME 'INLET1' /* NORMAL VELOCITY 4.0000E-01 */ W VELOCITY 4.0000E-01 K 3.2000E-04 EPSILON 1.5260E-05 TEMPERATURE 3.0500E+02 >>INLET BOUNDARIES PATCH NAME 'INLET2' /* NORMAL VELOCITY 6.0000E-01 */ W VELOCITY -6.0000E-01 K 7.2000E-04 EPSILON 5.1520E-05 TEMPERATURE 2.9500E+02 >>WALL BOUNDARIES PATCH NAME 'WALL1' TEMPERATURE 2.8800E+02 >>STOP