NACA 64015A Swept Back Wing
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2 Geometries
1 Mesh
2 Simulation setups
2 Results
2 Geometries 1 Mesh 2 Simulation setups 2 ResultsAbout this project
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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by Ali_ArafatAli_Arafat
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Adithya3090 created this project
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