Set up your own cloud-native simulation in minutes.Start Simulating Now
8AR, 0.6TR, 0.35aC
0
208
0
Statistics
1 Geometry
1 Mesh
1 Simulation setup
0 Results
About this project
Confirmation of XFLR5 results for a wing with 8AR, 0.6 taper ratio, and 0.35 average chord. Comparison of drag and lift results at 0 AOA with 20 m/s free stream velocity.
Related Projects
by Ali_ArafatAli_Arafat
Project History
nmok created this project