Similarly shaped airfoils to NPL 9615


New! Bulk download of polars in Excel format: npl9615.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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 9660
2. ONERA NACA CAMBRE
3. Ritz 1-30-12
4. NPL 9626
5. Horten 11.00% thick 1.00% camber
6. NPL 9627
7. MJZ1211
8. GIII BL45
9. NACA1412
10. GIII BL0
11. NACA64-212 a=0.0
12. NACA23012
13. RC-12(N)1
14. NACA63A112
15. NACA65-212 a=0.0
16. NACA64-212 a=0.2
17. NACA64A112
18. NACA63-212 a=0.0
19. AMES A-01
20. HAWKER TEMPEST 61% SEMISPAN
21. NACA63A111