Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm

<table>Effect of hole lateral angle on streamwise and spanwise <svg height="15.0875" id="M63" style="vertical-align:-2.3205pt" version="1.1" viewbox="0 0 73.587502 15.0875" width="73.587502" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> film cooling effectiveness for cooling hole forward angle of 15 deg and streamwise angle of 30 deg.</table>

International Journal of Aerospace Engineering

fig23

Figure 23

Figure 23: Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm 