Similarly shaped airfoils to NACA M27
New! Bulk download of polars in Excel format: m27.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 M24 (NACA-TR-221)
3. GOE 331 (PFALZ 60)
4. GOE 573
5. GOE 320 (HANSA-BRANDENBURG II.1)
6. GOE 366
7. GOE 14
8. GOE 364
9. GOE 630
10. GOE 15
11. GOE 322 (HANSA-BRANDENBURG IV.1)
12. NACA M24
13. EPPLER 422
14. GOE 562
15. CHEN
16. NACA M26
17. NACA M26 (NACA-TR-221)
18. NACA M21 (NACA-TR-221)
19. GOE 744
20. NACA M21
21. Horten 11.00% thick 10.00% camber