Similarly shaped airfoils to NACA M15
New! Bulk download of polars in Excel format: m15.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. NACA4312
3. NACA65-613 a=0.2
4. NACA64-613 a=0.2
5. GOE 285
6. BOEING 106
7. NACA65-612 a=0.2
8. NACA64-713 a=0.0
9. NACA65-713 a=0.0
10. NM Classic 12 root
11. CLARK-Y 11.7% smoothed
12. NACA63-613 a=0.2
13. EPPLER 334
14. GA 30A412
15. GOE 623
16. NACA65-712 a=0.0
17. NACA63-713 a=0.0
18. CLARK Y
19. NACA64-612 a=0.2
20. BOEING 103
21. FX 84-W-127