Similarly shaped airfoils to NACA63-710
New! Bulk download of polars in Excel format: NACA63-710.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
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2. NACA63-610 a=0.8
3. NACA64-610 a=0.8
4. HQ 3.5/10
5. NACA63A610
6. NACA65-710
7. NACA64A610
8. GOE 602 MOD.
9. RAF 32 MOD
10. NACA63-711
11. NACA63-709
12. MH 116 9.84%
13. NACA65-610 a=0.8
14. NACA64-709
15. NACA64-711
16. SG6042
17. EM J18 3510 26 51
18. AH 79-100 A
19. NACA63A609
20. HQ 3.5/9
21. MH 38 9.68%