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Urgent Help/3D Wing lift and drag
Posted 2021年10月26日 GMT-4 20:59 Structural & Acoustics, Fluid & Heat, Computational Fluid Dynamics (CFD) 2 Replies
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Hi, I hope everyone is doing good. I am solving 3D wing model and I am calculating lift and drag using the formulae. I am new to COMSOL. I am using following equations;
Lift= 2spf.T_stressy/(0.077257rho_infU_inf^2) ny(ny>0)+nz*(nz>0)
Drag = -2spf.T_stressz/(0.077257rho_inf*U_inf^2)
where my flow direction is -y direction and z axis is perpendicular direction (lift direction).
But I am not obtaining reasonable results. I hope your insights can help me accordingly. I have attaching some pictures of the sim file as well.
Thank you.