Similarly shaped airfoils to ONERA NACA CAMBRE
New! Bulk download of polars in Excel format: ncambre.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. NPL 9660
3. Ritz 1-30-12
4. NACA24012
5. MJZ1211
6. EPPLER 360
7. RC-12(N)1
8. AMES A-01
9. NPL 9627
10. EPPLER 361
11. NACA23012
12. NACA1412
13. Horten 12.00% thick 2.00% camber
14. GOE 766
15. NACA25012
16. NPL 9626
17. NACA64-212 a=0.2
18. Horten 11.00% thick 1.00% camber
19. TsAGI B 11.0% thick
20. NACA64-212 a=0.0
21. NACA63-212 a=0.2