Research Article

[Retracted] Research on Separation and Emission Reduction of Regional Airliner Based on Wake Encounter Response Model

Table 6

Maximum lift variation of longitudinal encountering double vortices.

Flight phaseMaximum lift position (m)Maximum lift variation at different separation (N)
7.49.311.113

Takeoff−6.7−87938.51−43850.85−23536.46−11334.77
Level flight−10.5−55549.54−28908.40−16236.23−8157.71
Landing−6.7−55954.09−27979.31−15116.82−7366.06