Engineering, 05.05.2020 05:38 alicegirl5133
The pressure distribution of the naca0012 airfoil at zero angles of attack. airfoil equations can be found on the handout posted on blackboard or from online sources. compare its pressure distribution with the experimental data (find references) using a) 10, b) 20, and c) 100 panels equally distributed on both top and bottom side (that means twice the number of panels). comment on your results in the form of a report on
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The pressure distribution of the naca0012 airfoil at zero angles of attack. airfoil equations can be...
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