Similarly shaped airfoils to HS 3.0/8


New! Bulk download of polars in Excel format: HS%203.0_8.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. Phoenix
2. LittleDevil
3. HS 3.0/9.0
4. S5020
5. HL75-K-3
6. NACA34007
7. NACA34009
8. NACA33007
9. Horten 9.00% thick 3.00% camber
10. NACA25107
11. FX 69-H-083
12. NACA35007
13. NACA63-409 a=0.2
14. Bartel 37 IIa 8%
15. FAD05
16. EPPLER 180
17. NACA63-509 a=0.0
18. HS 510
19. NACA64-409 a=0.2
20. Coanda 3
21. NACA63-409 a=0.0