Similarly shaped airfoils to NACA1410
New! Bulk download of polars in Excel format: NACA1410.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. HQ 1.0/10
3. SIKORSKY SC1095
4. EPPLER 226
5. NACA63A210
6. AIR 100-2 Acro MM 576 1999
7. NACA63-210
8. TP28-4
9. HM10011
10. Horten 10.00% thick 1.00% camber
11. NACA64-210
12. NACA1409
13. NACA63-210 a=0.0
14. HAWKER TEMPEST 96.77% SEMISPAN
15. NACA64A210
16. NACA63-210 a=0.2
17. NACA63A110
18. NACA63-211
19. NACA63-210 a=0.8
20. NACA64-210 a=0.0
21. NACA64-210 a=0.2