Set up your own cloud-native simulation in minutes.Start Simulating Now
morphing wing
126
0Statistics
2 Geometries
1 Mesh
1 Simulation setup
1 Result
2 Geometries 1 Mesh 1 Simulation setup 1 ResultAbout this project
this project will be used to to test out the aerodynamic efficiency of a partially morphed aerofoil with a gap between the stationary part and and partially morphed aerofoil with out a gap between the stationary section to see which one would be more useful for he future of aviation
Related Projects
by Ali_ArafatAli_Arafat
Project History
lnixon created this project