Similarly shaped airfoils to NACA23012
New! Bulk download of polars in Excel format: NACA23012.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (573) | 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. NACA22012
3. NACA32012
4. NACA22112
5. MJZ1211
6. NACA24112
7. Horten 12.00% thick 1.00% camber
8. NACA32112
9. Horten 12.00% thick 2.00% camber
10. NACA23013
11. ONERA NACA CAMBRE
12. NPL 9627
13. NPL 9626
14. GOE 766
15. NPL 9615
16. NACA23113
17. NPL 9660
18. Ritz 1-30-12
19. MH 106 13.07%
20. NACA32013
21. NACA22013