Similarly shaped airfoils to NACA64-410
New! Bulk download of polars in Excel format: NACA64-410.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA64-310 a=0.8
3. NACA63-310 a=0.8
4. NACA65-410
5. SB98 VS5 tip
6. HQ 2.0/10
7. CB2195
8. HQ 2.1/9.5
9. NACA64-310 a=0.6
10. SB99blks tip
11. NACA65-310 a=0.8
12. NACA63A310
13. NACA63-310 a=0.6
14. EM J8 2010 DrW
15. EM J18 2010
16. EM CY 1021 2010 X5 Fertig
17. NACA64A310
18. EM CY 1024 2010
19. SB99blkm mid
20. EM L5 2010
21. NACA65-310 a=0.6