Plot surface/3D plots using airfoil points and span at different wing stations.
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Hi,
I want to plot a wing using airfoil points and span. Alot of sources are availible for this case but my problem is a bit different. I have airfoil points and various wing station along span. Contours will be bassed on another matrix. I have tried to use surf(X,Y,Z,C) but it did't work.
for example:
x = [0 0.2 0.4 0.5 0.6 0.8 1 0.8 0.6 0.5 0.4 0.2 ]
z = [0 0.04 0.08 0.06 0.04 0.02 0 -0.02 -0.04 -0.06 -.0.08 -0.04]
spanwiseStations = linspace(0,2,10)
contour = rand(12,10)
Regards
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