Similarly shaped airfoils to NACA22013
New! Bulk download of polars in Excel format: NACA22013.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. NACA22013.5
3. NACA22113.5
4. NACA23013
5. Horten 13.00% thick 1.00% camber
6. NACA23113
7. NACA23013.5
8. NACA23113.5
9. NACA22014
10. NACA22012
11. NACA22112
12. NACA22114
13. NACA32013
14. Horten 14.00% thick 1.00% camber
15. NACA23014
16. BOEING 737 MIDSPAN
17. NACA32013.5
18. NACA23114
19. Horten 12.00% thick 1.00% camber
20. NACA23012
21. NACA32113