Similarly shaped airfoils to HQ 2.0/10
New! Bulk download of polars in Excel format: hq2010.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. EM J18 2010
3. EM J8 2010 DrW
4. SB99blkm mid
5. EM L5 2010
6. NACA63-410
7. EM CY 1021 2010 X5 Fertig
8. HQ 2.1/9.5
9. CB2195
10. SB99blkr root
11. SB98 VS5 tip
12. EPPLER 224
13. NACA64-410
14. EM CY 1024 2010
15. EM CY 1025 20098
16. HN-808
17. FAD14
18. NACA63-310 a=0.8
19. SB95 9.5/2
20. EM J18 2310
21. NACA63-310 a=0.6