Similarly shaped airfoils to HS 3.0/9.0
New! Bulk download of polars in Excel format: HS%203.0_9.0.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
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. Horten 9.00% thick 3.00% camber
3. Phoenix10
4. HS 3.0/8
5. Phoenix
6. JWL079 9.7/2.7
7. FAD23
8. NACA33009
9. NACA35009
10. NACA25109
11. NACA34010
12. NACA35010
13. NACA34109
14. Horten 9.00% thick 4.00% camber
15. NACA63-409 a=0.2
16. S5010
17. FX 69-H-083
18. NACA63-409 a=0.0
19. NACA44009
20. NACA64-409 a=0.2
21. NACA63-509 a=0.0