NLLL: Non-Linear Lifting Line Solver

Manual

Airfoil ClCdCm Database

Convergence Tips

                 

# Alpha:       Alpha min:       Alpha max:      

Reference Area:           Reference Length:      

Reference Point:     x:   y:   z:  

Symmetry Plane at y=0             Ground Plane at z=

Relaxation Factor:         Tolerance:             Max Iterations:

Dissipation:         k2:         k4:        


Surface 1:               # panels:               dist:

       
Root:         xc/4:     yc/4:     zc/4:    
Tip:         xc/4:     yc/4:     zc/4:    

Root:         chord:       twist:       flap:       section:      
Tip:         chord:       twist:       flap:       section:      


Surface 2:               # panels:               dist:

       
Root:         xc/4:     yc/4:     zc/4:    
Tip:         xc/4:     yc/4:     zc/4:    

Root:         chord:       twist:       flap:       section:      
Tip:         chord:       twist:       flap:       section:      





Generate New Input Form

Number of surfaces:   (maximum 10)

                           

Run Using Input File