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

Table 8

Maximum value of double vortex rolling moment encountered.

Flight phase	Maximum position	Variation of rolling torque at different separation
		7.4	9.3	11.1	13
Takeoff	−14.5	79753.67	39764.82	21342.73	10278.22
	0	−348878.42	−173949.19	−93362.73	−44961.55
Level flight	−14.2	81640.60	41735.04	23440.23	11777.28
	0	−291611.09	−149072.95	−83725.91	−42067.16
Landing	−14.1	68380.62	34181.28	18467.31	8998.62
	0	−259737.77	−129871.20	−70166.46	−34190.25