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

バージョン 1.0.0.0 (116 KB) 作成者: sunil anandatheertha
Generate coordinates for slotted ClarkY airfoil having leading edge slat and trailing flap.
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ダウンロード: 869
更新 2012/2/3

ライセンスの表示

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

引用

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. 取得済み .

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

バージョン 公開済み リリース ノート
1.0.0.0