Similarly shaped airfoils to NPL 9627


New! Bulk download of polars in Excel format: npl9627.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
Dynamic plotter New!
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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. NPL 9626
2. NACA1412
3. Ritz 1-30-12
4. MJZ1211
5. NPL 9615
6. NPL 9660
7. ONERA NACA CAMBRE
8. NACA23012
9. HQ 1.0/12
10. AMSOIL2 RUTAN WING
11. S8038 (13%)
12. Horten 12.00% thick 1.00% camber
13. NACA63A112
14. HAWKER TEMPEST 61% SEMISPAN
15. NACA22012
16. NACA63-213 a=0.0
17. NACA64-213 a=0.0
18. NACA63-213 a=0.2
19. NACA63A113
20. NACA63A212
21. NACA63-213