Research Article
[Retracted] Research on Separation and Emission Reduction of Regional Airliner Based on Wake Encounter Response Model
Table 9
Maximum rolling moment coefficient.
| | Flight phase | Maximum position | Maximum rolling moment coefficient at different separation | | 7.4 | 9.3 | 11.1 | 13 |
| | Takeoff/single vortex | 0 | −0.1292 | −0.0644 | −0.0346 | −0.0166 | | Level flight/single vortex | 0 | −0.0931 | −0.0476 | −0.0267 | −0.0133 | | Landing/single vortex | 0 | −0.0821 | −0.0411 | −0.0222 | −0.0108 | | Takeoff/twin vortex | 0 | −0.1325 | −0.0661 | −0.0355 | −0.0171 | | Level flight/double vortex | 0 | −0.1107 | −0.0398 | −0.0318 | −0.0160 | | Landing/double vortex | 0 | −0.0987 | −0.0566 | −0.0267 | −0.0130 |
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