https://github.com/sukhbinder/nacaaerofoil

Python binding for fortran code to generate naca symmetric and cambered aerofoil
https://github.com/sukhbinder/nacaaerofoil

Last synced: about 2 months ago
JSON representation

Python binding for fortran code to generate naca symmetric and cambered aerofoil

• Host: GitHub
• URL: https://github.com/sukhbinder/nacaaerofoil
• Owner: sukhbinder
• Created: 2014-09-12T14:43:57.000Z (over 10 years ago)
• Default Branch: master
• Last Pushed: 2014-09-12T15:18:28.000Z (over 10 years ago)
• Last Synced: 2023-08-06T04:51:56.521Z (over 1 year ago)
• Language: FORTRAN
• Size: 109 KB
• Stars: 0
• Watchers: 2
• Forks: 0
• Open Issues: 0
• Metadata Files:
  • Readme: README.md

Awesome Lists containing this project

README

        
	

#Aerofoil Naca

naca4_sym(c,t,n) evaluates y(x) for a NACA symmetric 4-digit airfoil.

C the chord length.

T the maximum relative thickness.

N the number of sample points.

	

naca4_cam(m,p,t,c,n) Generates (xu,yu), (xl,yl) for a NACA cambered 4-digit airfoil.

M, the maximum camber.

P, the location of maximum camber.

T, the maximum relative thickness.

C, the chord length.

N, the number of sample points.

	

python wrapper for the code by  John Burkardt

by Sukhbinder Singh