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Table A3.

Time step refinement study results for a NACA 0013 aerofoil moving at a Reynolds number of 6000 when 0.1 body lengths away from the wall

Time step refinement study results for a NACA 0013 aerofoil moving at a Reynolds number of 6000 when 0.1 body lengths away from the wall
Time step refinement study results for a NACA 0013 aerofoil moving at a Reynolds number of 6000 when 0.1 body lengths away from the wall
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