Similarly shaped airfoils to NACA6718
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. NACA6717
3. NACA6716
4. NACA6720
5. GOE 646
6. NACA6715
7. GOE 223 (MVA H.34)
8. EPPLER 748
9. EPPLER 857
10. GOE 255 (MVA CA.6)
11. GOE 229 (MVA H.39)
12. Joukowsky 19.00% thick 6.00% camber
13. Joukowsky 20.00% thick 6.00% camber
14. GOE 620
15. GOE 797
16. GOE 692
17. NACA63A718
18. GOE 420
19. Joukowsky 18.00% thick 6.00% camber
20. Joukowsky 19.00% thick 5.00% camber
21. NACA63A719