International Journal of Aerospace Engineering / 2009 / Article / Tab 3

Research Article

Turbine Airfoil Optimization Using Quasi-3D Analysis Codes

Table 3

Design variables.

NameLower boundUpper boundInitial valueFinal value

peak_exit01.31.152391.09774
peak_exit_loc0.610.6552260.702005
peak_imin01.53.849031.63175
rad_le0.03550.01772450.0177331
Wedge26.62.38372.87872
Ugt51816.000412.2213
Te0300.02991020.0299102
Ovt 43.222231.77036
Stagger05030.960339.1863
Deltal 30
Tmax020.1412410.138897
tmax_c0.040.20.0942850.0837007
Pctz020.3895310.40175
Carea0100.1650280.174538

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