Similarly shaped airfoils to HQ 1.5/10


New! Bulk download of polars in Excel format: hq1510.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 CY 1016 1510
2. NACA63-310
3. NACA64-310
4. TP-CIEL-S
5. TP210-10%
6. SB96VS 9.75/1.25
7. RG 14 9.5%
8. AIR 100-2 Acro MM 576 1999
9. HN-1069c
10. GA 35-210
11. RG 14 10%
12. TPR-95-96-95
13. GA 37-210
14. GA 35A210
15. NM20 root
16. RG-12
17. GA 30-210
18. RAE 5213
19. NACA63-210 a=0.6
20. NACA63-210 a=0.8
21. RAF 28