Table 6

Comparison of main aerodynamic properties of wings BASELINE-S340 and WS-FUS-S340-B

Aerodynamic propertyBASELINE-S340WS-FUS-S340-BImprovement (%)
CL1.5/CD @ CL = 0.9622.04522.8743.8
CL/CD @ CL = 0.9622.52623.3613.7
CL max1.3981.4322.4
Source: Table by authors

or Create an Account

Close subscription notice
Close access options