Similarly shaped airfoils to NACA M11
New! Bulk download of polars in Excel format: m11.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. NACA M5
3. JWL066 8.7/1.9
4. JWL075 8.8/1.76
5. DD928416
6. GIII BL387
7. GIII BL430
8. RG 14
9. NACA2209
10. NACA64-309 a=0.0
11. NACA64-309 a=0.2
12. NACA25009
13. GIII BL369
14. NACA2309
15. B-29 TIP
16. NACA63-309 a=0.0
17. NACA63-309 a=0.2
18. MH 20 9.01%
19. NACA65-309 a=0.0
20. BOEING 707 .54 SPAN
21. SM8516m