Similarly shaped airfoils to NACA23110
New! Bulk download of polars in Excel format: NACA23110.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
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2. NACA32010
3. NACA23010.5
4. Horten 10.00% thick 2.00% camber
5. NACA32110
6. NACA24110
7. NACA24010
8. NACA32010.5
9. BOEING-VERTOL V23010-1.58
10. NACA23110.5
11. HM391-2
12. NACA24110.5
13. NACA42010
14. NACA24010.5
15. ONERA OA209
16. LOCKHEED-GEORGIA SUPERCRITICAL
17. NACA32110.5
18. EH 2.0/10
19. NACA23109
20. NACA42010.5
21. NACA23009