Similarly shaped airfoils to NACA M15 (NACA-TR-221)
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
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2. NACA M18
3. NACA M18 (NACA-TR-221)
4. NACA65-613 a=0.2
5. NACA64-613 a=0.2
6. NACA65-612 a=0.2
7. NACA65-613 a=0.0
8. NACA64-713 a=0.0
9. NACA45012
10. NACA63-613 a=0.2
11. EPPLER 334
12. NACA4312
13. BOEING 106
14. NACA65-612 a=0.0
15. NACA64-613 a=0.0
16. NACA65-713 a=0.0
17. NACA64-612 a=0.2
18. NACA63-713 a=0.0
19. GA 30A412
20. NACA45013
21. Ritz 3-30-12