Similarly shaped airfoils to NM08


New! Bulk download of polars in Excel format: NM08.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. TP29-7%
2. HT13
3. S1010 HPV airfoil
4. NACA0006
5. TP96-0.5%
6. HQ 0/7
7. FAD07
8. SC(2)-0406
9. BOEING-VERTOL VR-9
10. EPPLER EA 8(-1)-006
11. SC(2)-0606
12. S8025 (8%)
13. HN-968S
14. NACA M1
15. NACA M1 (NACA-TR-221)
16. SC(2)-0706
17. GOE 445
18. PW2019 tip airfoil 3m
19. TP96-0.75%
20. HN-311S
21. RAF 30 MOD