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

Table 7

Variation of maximum rolling moment of single vortex encountered in longitudinal direction.

Flight phase	Maximum rolling moment position	Variation of maximum rolling moment at different separation
		7.4	9.3	11.1	13
Takeoff	14.7	97718.75	48721.65	26150.03	12593.30
	0	−340145.25	−169594.98	−91025.73	−43836.10
Level flight	14.7	74058.84	37859.21	21263.39	10678.62
	0	−245234.25	−125364.87	−70410.40	−35274.49
Landing	14.7	62173.50	31086.72	16795.38	8183.92
	0	−216418.26	−108209.72	−58463.09	−28487.48