Similarly shaped airfoils to HQ 3.0/10


New! Bulk download of polars in Excel format: hq3010.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. EM J8 3010 DrW
2. NACA63-610
3. EM J19 3010
4. NACA64-610
5. NACA63-510 a=0.8
6. SB96 10.5/3.0
7. NACA64-510 a=0.8
8. NACA63A510
9. S7075 (9%)
10. NACA64A510
11. GOE 595
12. EM J18 3010 26 51
13. EPPLER E193gU-K24
14. NACA63-611
15. S3024 9.84%
16. GA 35-410
17. HQ 3.0/9
18. NACA63-510 a=0.6
19. GA 37-410
20. NACA65-610
21. GOE 602