Table 7

Comparison of main aerodynamic properties of wings BASELINE-J170 and WS-FUS-J170-C

Aerodynamic propertyBASELINE-S170WS-FUS-S170-AImprovement (%)
CL1.5/CD @ CL = 1.1219.32320.4075.6
CL/CD @ CL = 1.1218.26619.2955.6
Source: Table by authors
[ViewLarge]
This Feature Is Available To Subscribers Only

or Create an Account

Close subscription notice
Close access options