Similarly shaped airfoils to CLARK YS


New! Bulk download of polars in Excel format: clarkys.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. NACA25112
2. NACA 2R212
3. NACA CYH
4. Horten 12.00% thick 3.00% camber
5. NACA M6 (NACA-TR-221)
6. NACA M6
7. ZAGI 12
8. EH 3.0/12
9. TsAGI B 12.0% thick
10. TsAGI B 11.5% thick
11. EPPLER 331
12. NACA25113
13. EH 2.0/12
14. Horten 13.00% thick 3.00% camber
15. RAF 34
16. ONERA OA212
17. NACA33012
18. Horten 11.00% thick 3.00% camber
19. NACA25012
20. EPPLER 635
21. GOE 677 (= M 6)