Turbine Airfoil Optimization Using Quasi-3D Analysis Codes

<table>Change in objective function for low-pressure turbine nozzle optimization using gradient-based search (ADS <svg height="7.6374998" id="M92" style="vertical-align:-0.0pt" version="1.1" viewbox="0 0 22.012501 7.6374998" width="22.012501" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,2.9,7.575)"><path d="M901 255q-71 -62 -185 -187l-22 15l102 147h-727v50h727l-102 147l22 15q114 -125 185 -187z" id="x2192"></path></g>
</svg> Istrat = 0, Iopt = 1, Ioned = 1).</table>

International Journal of Aerospace Engineering

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Figure 16

Figure 16: Turbine Airfoil Optimization Using Quasi-3D Analysis Codes 