Approach and Landing Aircraft Wake Encounter Risk Based on Reynolds-Averaged Navier-Stokes Numerical Simulation

<div>The force of the ARJ21 aircraft encountering the wake. (a) Two-dimensional plane coordinate system of the wake encountered by the following aircraft. (b) The vertical velocity distribution of the wake vortex of the B-H model in the spanwise direction.</div>

International Journal of Aerospace Engineering

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Figure 12

Figure 12: Approach and Landing Aircraft Wake Encounter Risk Based on Reynolds-Averaged Navier-Stokes Numerical Simulation 