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Table A2.

Mesh refinement study results for an axisymmetric body of revolution based on a NACA 0013 aerofoil at a Reynolds number of 6000 in open water

Mesh refinement study results for an axisymmetric body of revolution based on a NACA 0013 aerofoil at a Reynolds number of 6000 in open water
Mesh refinement study results for an axisymmetric body of revolution based on a NACA 0013 aerofoil at a Reynolds number of 6000 in open water
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