Similarly shaped airfoils to GA 35A316


New! Bulk download of polars in Excel format: GA%2035A316.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 37A316
2. GA 40A316
3. GA 40-316
4. GA 37-316
5. NACA63A416
6. GEMINI (smoothed)
7. NACA64A416
8. NACA65-416 a=0.5
9. NACA65-416 a=0.6
10. GA 37-317
11. NACA64-416 a=0.5
12. GA 35A315
13. NACA64-416 a=0.6
14. GA 35A317
15. MB253515 15.0% smoothed
16. GA 37A317
17. RONCZ 1082T VOYAGER TIP OUTER AFT WING
18. GA 37A315
19. GA 30-316
20. GA 35-316
21. CB2515