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September 27, 2017, 05:59
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URGENT! help needed
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New Member
jonathan
Join Date: Sep 2017
Posts: 1
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hi, im a student doing a project on NACA 4424 aerofoil. i just started using ANSYS for my simulation. However i was faced with numerous challenges, i would like to ask for your kind assistance.
i am trying to aquire the lift and drag coefficient of the aerofoil at various angle of attack (AOA) -8, -4, 0, 4, 8, 12, 16. Thank you so much, hope to hear from you guys soon. |
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