Similarly shaped airfoils to NPL 9626
New! Bulk download of polars in Excel format: npl9626.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. Ritz 1-30-12
3. NACA63A112
4. MJZ1211
5. NACA1412
6. NPL 9615
7. Horten 12.00% thick 1.00% camber
8. NPL 9660
9. NACA22012
10. NACA64A112
11. NACA23012
12. NACA63A113
13. HAWKER TEMPEST 61% SEMISPAN
14. NACA64-112 a=0.2
15. NACA64-112 a=0.5
16. NACA63-112 a=0.2
17. NACA63-112 a=0.5
18. AMSOIL2 RUTAN WING
19. NACA64-112 a=0.6
20. GIII BL0
21. NACA63-112 a=0.6