Power Fan Design of Blended-Wing-Body Aircraft with Distributed Propulsion System

Figure 10

Aircraft pressure nephogram and velocity distribution on the upper surface of power system fairing under different flow rates. (a) The intake flow is 810 kg/s. (b) The intake flow is 984 kg/s. (c) Fairing velocity distribution at 810 kg/s. (d) Fairing velocity distribution at 984 kg/s.

(a)

(b)

(c)

(d)