Experimental Investigations on Aircraft Blade Cooling Holes and CFD Fluid Analysis in Electrochemical Machining

<div>Cooling hole samples machined under different applied voltages. (a) U = 5 V, ξ = 5% (wt.%). (b) U = 9 V, ξ = 5% (wt.%). (c) U = 13 V, ξ = 5% (wt.%).</div>

Advances in Materials Science and Engineering

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Figure 6

Figure 6: Experimental Investigations on Aircraft Blade Cooling Holes and CFD Fluid Analysis in Electrochemical Machining 