Similarly shaped airfoils to HQ 3.0/12


New! Bulk download of polars in Excel format: hq3012.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 J18 3012 DrW r1,2
2. EM J18 3212
3. NACA63-612
4. NACA64-612
5. NACA63-512 a=0.8
6. NACA64-512 a=0.8
7. SB 96 12.7/3.0
8. EM L3 3012
9. SB96 11.6/3.0
10. NACA63A512
11. NACA63-613
12. HQ 3.0/11
13. HQ 3.0/13
14. SBC3
15. EPPLER 201
16. NACA64-613
17. NACA63-513 a=0.8
18. CLARK X
19. GA 35-412
20. CLARK K
21. NACA63-512 a=0.6