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2 Geometries
1 Mesh
1 Simulation setup
1 ResultCFD 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
by slilbaekslilbaek
Adithya3090 created this project
over 10 years ago
2 Geometries 1 Mesh 1 Simulation setup 1 ResultCFD 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
