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
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. 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