Similarly shaped airfoils to GIII BL0
New! Bulk download of polars in Excel format: giiia.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 9615
3. NPL 9660
4. R140 (original)
5. R140 12.04% (smoothed)
6. NACA22012
7. NPL 9626
8. NACA22112
9. NACA65-112 a=0.0
10. Horten 12.00% thick 1.00% camber
11. NACA65-112 a=0.2
12. N-14
13. NACA64A112
14. N-12
15. NACA63A112
16. NACA65-111 a=0.0
17. NACA64-112 a=0.0
18. NACA66-111 a=0.0
19. NACA65-111 a=0.2
20. NACA64-012A
21. NACA65A111