Similarly shaped airfoils to NACA65-518
New! Bulk download of polars in Excel format: NACA65-518.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. NACA64A418
3. NACA65-418 a=0.6
4. GA 40-318
5. GA 40A318
6. NACA65-519
7. NACA65-517
8. NACA65-417 a=0.8
9. NACA63A418
10. NACA65-419 a=0.8
11. NACA65-418
12. NACA65-618
13. NACA65-418 a=0.5
14. NACA64-518
15. LS(1)-0417 (GA(W)-1)
16. NACA64A417
17. GA 37A318
18. NACA65A418
19. NACA64-418 a=0.8
20. NACA64(3)-418
21. NACA65A417