Plane flying

8Kg Payload - 36KG MTOW

36KG MTOW plane

36Kg MTOW, 8Kg payload plane

System specification from mission profile

Given the mission profile, we determine the velocites and accelerations that the plane should handle Based on that VN diagram is made

VN diagram for plane

Flight envelop graph - giving loadfactor for the Velocities required my mission profile

Given the mission profile, To achieve required lift in all the scenarios - (take off, landing, cruise speed, climb, max speed, banking/turning …)

Wing area sizing for the plane

Wing area sizing according to mission requirements

Sample of wing optimization using XFLR5

Blended wing GE concept

Blended wing Ground effect concept

Pathlines from blended wing surface - CFD showing forward swept wing characteristics

Validation CFD Cases

Validation case for 0 aoa NACA0012 airfoil

Validation case for 0 aoa NACA0012 airfoil

Mesh used in the study

Validation case - mesh used for the study

Validation case for higher aoa

Validation case for high lift generation