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[venkyvenkatesh374]

Hello All,

 

I have uploaded two snips case 1 and case 2.,

In case 1 wing is flat and velocity is at 7deg angle., i.e., cartesian x and z components, lift generated is 248N,

In case 2 wing is tilted to 7deg, velocity is normal to boundary, Lift generated is 550N,

I don't know where am making wrong sir., please help me out.

 

[abhishek.roy]

Lift force is perpendicular to chord. So the first case where wing is flat force on Z axis is lift force. In second case where wing is tilted force on Z axis is not lift.