Comparison of main aerodynamic properties of wings BASELINE-S170 and WS-FUS-S170-A
| Aerodynamic property | BASELINE-S170 | WS-FUS-S170-A | Improvement (%) |
|---|---|---|---|
| CL1.5/CD @ CL = 0.96 | 24.203 | 25.025 | 3.4 |
| CL/CD @ CL = 0.96 | 24.721 | 25.557 | 3.4 |
| CL max | 1.309 | 1.407 | 7.5 |
| BASELINE-S170 | WS-FUS-S170-A | Improvement (%) | |
|---|---|---|---|
| 24.203 | 25.025 | 3.4 | |
| 24.721 | 25.557 | 3.4 | |
| 1.309 | 1.407 | 7.5 |
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