Similarly shaped airfoils to N-22
New! Bulk download of polars in Excel format: n22.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (11) | 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. N-10
3. Curtis C-72
4. USA-35B
5. NACA CYH
6. Dayton-Wright T-1
7. Rhode St. Genese 34
8. Horten 13.00% thick 4.00% camber
9. NACA44013
10. Horten 12.00% thick 4.00% camber
11. NACA44013.5
12. CLARK YS
13. NACA35013
14. NACA35113
15. NACA35012
16. NACA34013
17. NACA35112
18. NACA34113
19. NACA34112
20. Horten 12.00% thick 3.00% camber
21. NACA34012