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Fig. 10 | Advances in Aerodynamics

Fig. 10

From: Flight simulation from takeoff to yawing of eVTOL airplane with coaxial propellers by fluid-rigid body interaction

Fig. 10

Snapshots of flow fields (Isosurface of velocity magnitude \(10 \mathrm {~m/s}\)) around the aircraft during takeoff in the case where the target altitude is \(12\mathrm {~m}\): left at \(t = 0.72 \mathrm {~s}\), right at \(t = 1.76 \mathrm {~s}\). Wind of \(10 \mathrm {~m/s}\) reached a maximum distance of \(16.9\mathrm {~m}\) away from the center of the aircraft (One unit of ground scale is \(2\mathrm {~m}\))

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