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
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.
2. NACA 2R212
3. NACA CYH
4. Horten 12.00% thick 3.00% camber
5. NACA M6
6. ZAGI 12
7. EH 3.0/12
8. TsAGI B 12.0% thick
9. TsAGI B 11.5% thick
10. EPPLER 331
11. NACA25113
12. EH 2.0/12
13. Horten 13.00% thick 3.00% camber
14. RAF 34
15. ONERA OA212
16. NACA33012
17. Horten 11.00% thick 3.00% camber
18. NACA25012
19. EPPLER 635
20. GOE 677 (= M 6)
21. TsAGI B 12.5% thick