International Journal of Aerospace Engineering / 2009 / Article / Tab 2

Research Article

Turbine Airfoil Optimization Using Quasi-3D Analysis Codes

Table 2

Constrained variables used in the formulation of the airfoil design problem.

Constrained variableLower boundUpper bound

peak_exit01.3
peak_exit_loc0.61
peak_imin01.5
Carea010
rad_le0.0355
Wedge26.6
Te030
Ovt−14
delta1−3030
tmax_c0.040.2
Pctz02

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