Similarly shaped airfoils to GA 37A316


New! Bulk download of polars in Excel format: GA%2037A316.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 35A316
2. GA 40A316
3. GA 40-316
4. NACA65-416 a=0.5
5. NACA65-416 a=0.6
6. NACA64A416
7. RONCZ 1082T VOYAGER TIP OUTER AFT WING
8. NACA63A416
9. GEMINI (smoothed)
10. GA 37A315
11. GA 37A317
12. GA 37-316
13. GA 40A317
14. MB253515 15.0% smoothed
15. NACA65-416 a=0.8
16. GA 35A315
17. NACA65-516
18. GA 40-317
19. GA 35A317
20. GA 37-317
21. NACA64-416 a=0.5