International Journal of Aerospace Engineering / 2009 / Article / Tab 4

Research Article

Turbine Airfoil Optimization Using Quasi-3D Analysis Codes

Table 4

Objective function components.

ParameterWeightInitial valueFinal value

dev_suction100.1770970.0644436
dev_pressure2.50.0450l370.0112053
diff_suction50.1869320.128518
diff_pressure1.50.3085360.0656558
le_crossover5000
le_smoothness2.50.00350420.00875813
peak_exitl.9005l.80434
peak_exit_loc00
peak_imin12.2872.43818
Carea0.2129210.225093
tmax/c00
Wedge00
Ugt00
Ovt00
Objective function value18.46536.53994

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