Set up your own cloud-native simulation in minutes.Start Simulating Now
Front wing Design
252 0
Statistics
2 Geometries 2 Meshes 2 Simulation setups 2 Results
About this project
To 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.
Related Projects
Project History
Sunish created this project