Explore agentic engineering workflow on SimScaleExperience Engineering AI
NACA 64015A Swept Back Wing
404
0
Statistics
2 Geometries
1 Mesh
1 Simulation setup
2 Results
2 Geometries 1 Mesh 1 Simulation setup 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
