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2 Geometries
2 Meshes
2 Simulation setups
2 ResultsTo investigate the behavior of drag and lift and determine the stall zone for two different front wing flap angles: 6 degrees (standard) and 18 degrees (high downforce) considering a constant inlet velocity of 20 m/s.
by simscalesimscale
Sunish created this project
almost 9 years ago
2 Geometries 2 Meshes 2 Simulation setups 2 ResultsTo investigate the behavior of drag and lift and determine the stall zone for two different front wing flap angles: 6 degrees (standard) and 18 degrees (high downforce) considering a constant inlet velocity of 20 m/s.
