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Generate coordinates for slotted ClarkY airfoil having leading edge slat and trailing flap

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Generate coordinates for slotted ClarkY airfoil having leading edge slat and trailing flap.

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use wordpad to open the dat files

LIST OF FILES CONTAINED

1. AirfoilSection.jpeg

2. airfoil_new.m -->>> main file
3. loadairfoilCY.m
4.loadnaca23012.m

5. Flap.dat ---- OUTPUT
6. MainWingClarkY.dat ---- OUTPUT
7. SlatDimensions.dat ---- OUTPUT

8. airfoil_1.wmf
9. complete wing.wmf
10. plane.wmf
11. top view.wmf
12. READ ME.rtf

FILES NEEDED -- you have to get them from these links:
13. http://naca.central.cranfield.ac.uk/reports/1933/naca-report-427.pdf
14. http://www.arvelgentry.com/amo/High-Lift_Aerodynamics.pdf

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Clark Y airfoil with front slat(a section of CY) and flap(naca 23012)/