Similarly shaped airfoils to NACA23010
New! Bulk download of polars in Excel format: NACA23010.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (30) | 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. NACA23010.5
3. BOEING-VERTOL V23010-1.58
4. NACA24010
5. NACA32010
6. Horten 10.00% thick 2.00% camber
7. LOCKHEED-GEORGIA SUPERCRITICAL
8. NACA24010.5
9. ONERA OA209
10. Sipkill 1.7/10
11. NACA32010.5
12. NACA24110
13. HM391-2
14. EH 2.0/10
15. NACA25010
16. TsAGI B 9.5% thick
17. NACA23009
18. BOEING VERTOL V(1.95)3009-1.25
19. NACA32110
20. Ritz 1-30-10
21. NACA24110.5