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Boundary Conditions and Optimization Settings<br />

Rolls-Royce high pressure compressor stator blade mid-section<br />

inlet flow conditions<br />

Ma= 0.776<br />

α I<br />

= 46.8°<br />

T 0<br />

= 447K<br />

P 0<br />

= 439 kPa<br />

Re =1.09E+06<br />

Tu = 4%<br />

optimization strategy<br />

algorithm: NSGA-II<br />

number of individuals: 50<br />

number of generations: 200<br />

computational environment<br />

CPU: 1x Pentium IV<br />

Speed: 3.6 GHz<br />

RAM: 3 GB<br />

ERCOFTAC 2006, April 5-75<br />

7

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