Similarly shaped airfoils to GA 35A318


New! Bulk download of polars in Excel format: GA%2035A318.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
Dynamic plotter New!
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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1. GA 37A318
2. GA 40A318
3. NACA63A418
4. GA 40-318
5. GA 37-318
6. NACA64A418
7. GA 35A319
8. GA 35A317
9. GA 37-319
10. NACA65-418 a=0.5
11. NACA65-418 a=0.6
12. GA 37A319
13. GA 37A317
14. NACA64-418 a=0.6
15. GA 30-318
16. NACA64-418 a=0.5
17. GA 30-317
18. GA 40A319
19. GA 35-318
20. NACA64-419 a=0.6
21. NACA65-518