NACA profile for ANSYS | NACA profile using Python | Python for mechanical engineer

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The NACA airfoils are airfoil shapes for aircraft wings developed by the National Advisory Committee for Aeronautics (NACA). The shape of the NACA airfoils is described using a series of digits following the word "NACA". The parameters in the numerical code can be entered into equations to precisely generate the cross-section of the airfoil and calculate its properties.

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Sir I 'm a aerospace engineering student I need your help.. I have code for NACA 0012 airfoil but I don't know it's correct or not.... Please help me 🙏🙏

sandhyabesra
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sir can u plzz tell me which python labraries should i learn as mechanical engineer . bcoz sir i have completed my basic course on python .

is-ckqy
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Hello i am student and i do need your help in fusion 360
I have problem to solve but i can not .. Can we chatting on Email to send you the geometry please

omer-ayed
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