Showing posts with the label aerodynamics graph plotting in pythonShow all
python airfoil
naca airfoil ploting in matplotlib python
Naca airfoil ploting in matplotlib python Code: from matplotlib.pyplot import * from numpy import * t = .2 c= 1.5 xc = linspace(0,1,100) y1 = t*c/.2*(.296*sqrt(xc)-.12…
Read more
- Engineer Know
- i am a mechanical engineer who don't know what i am doing with life so i am trying to earn some bucks with this blog
Social Plugin