Similarly shaped airfoils to NACA M25
New! Bulk download of polars in Excel format: m25.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.
2. NACA M26 (NACA-TR-221)
3. NACA M26
4. GOE 265
5. M 77
6. NACA M22 (NACA-TR-221)
7. NACA M23 (NACA-TR-221)
8. NACA M22
9. GOE 207 (AVIATIK V8)
10. NACA M9
11. NACA M19
12. GOE 15
13. GOE 300 (FRIEDRICHSHAFEN G20)
14. GOE 381
15. GOE 417
16. NACA M19 (NACA-TR-221)
17. NACA M8
18. NACA M23
19. NACA M20
20. GOE 402
21. GOE 173 (ALBATROS 6020)