Research Article

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

Table 10

Calculation results of the longitudinal characteristics of outflow flow field.


0−0.14420.01550.0448−9.30323
30.36180.01600.005022.5949
50.71750.0373−0.034519.2359
70.90000.0802−0.034611.2220
100.95000.16000.01005.9375

Note: is the angle of attack. is the lift coefficient. is the drag coefficient. is the moment coefficient. is the lift-to-drag ratio.