Generate coordinates for slotted ClarkY airfoil having leading edge slat and trailing flap
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
Zitieren als
sunil anandatheertha (2024). Generate coordinates for slotted ClarkY airfoil having leading edge slat and trailing flap (https://www.mathworks.com/matlabcentral/fileexchange/34912-generate-coordinates-for-slotted-clarky-airfoil-having-leading-edge-slat-and-trailing-flap), MATLAB Central File Exchange. Abgerufen .
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- Industries > Aerospace and Defense > Airfoil tools >
- Engineering > Aerospace Engineering > Aerodynamics >
- Aerospace > Aerospace Toolbox > Standard Workflow Procedures > Coordinate Systems >
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Clark Y airfoil with front slat(a section of CY) and flap(naca 23012)/
Version | Veröffentlicht | Versionshinweise | |
---|---|---|---|
1.0.0.0 |