Fig. 1.

Fig. 2.

Fig. 3.

Fig. 4.

Fig. 5.

Fig. 6.

Fig. 7.

Fig. 8.

Fig. 9.

Fig. 10.

Fig. 11.

Fig. 12.

Fig. 13.

Summary of distributed propulsion concepts analyzed in the current work_
| Concept name | Description | |
|---|---|---|
| a) | Baseline | Single pusher propeller located behind the fuselage. |
| b) | Prop 1 | Row of five small propellers in front of each aft wing. |
| c) | Prop 2 | Row of five small propellers behind each aft wing. |
| d) | Hybrid | Three small propellers added behind of each aft wing. |
| e) | EDF1 | Row of five ducted fans on each aft wing. |
| f) | EDF2 | Row of five ducted fans behind each aft wing. |