International Journal of Aerospace Engineering / 2009 / Article / Tab 5

Research Article

Turbine Airfoil Optimization Using Quasi-3D Analysis Codes

Table 5

Constraint variables.

NameLower boundUpper boundInitial valueFinal value

c10.20.50.350.35
c20.250.750.50.632109
c30.250.750.50.569811
Tmaxx0.050.150.1395160.139516
Stagger84031.64339.4644
Pcttle 0.2500
Ratl041.252.7032
Ratu042.594422.72716
Ti010.51
E1532.04457

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