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
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. NACA M11 (NACA-TR-221)
2. BOEING-VERTOL VR-14
3. NACA M5
4. JWL066 8.7/1.9
5. JWL075 8.8/1.76
6. DD928416
7. GIII BL387
8. GIII BL430
9. RG 14
10. NACA2209
11. NACA64-309 a=0.0
12. NACA64-309 a=0.2
13. NACA25009
14. GIII BL369
15. NACA2309
16. B-29 TIP
17. NACA63-309 a=0.0
18. NACA63-309 a=0.2
19. MH 20 9.01%
20. NACA65-309 a=0.0
21. BOEING 707 .54 SPAN