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Table 1 The percentage of reduction after inserting the holes

From: Shape optimization of turbine blade cooling system using topological sensitivity analysis method

Test cases

Creating one hole

Creating two holes

Creating multiple holes

j(Ω)

\( 1230\ 10^{3} \)

\( 1230\ 10^{3} \)

\( 1230\ 10^{3} \)

\(j(\varOmega \backslash \overline{\mathcal{H}})\)

\( 753\ 10^{3} \)

\( 639\ 10^{3} \)

\( 438\ 10^{3} \)

Percentage of reduction

38%

48%

64%