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NACA 64015A Swept Back Wing

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j_martins
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CFD analysis to verify the experimental results carried out on NACA 64015A Swpetback wing at AoA zero degree and Sweep angle 20 degrees. Reference: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980227185.pdf

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  • Adithya3090

    Adithya3090 created this project

  • j_martins

    j_martins copied this project