Similarly shaped airfoils to GA 37A419
New! Bulk download of polars in Excel format: GA%2037A419.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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2. GA 40A419
3. GA 40-419
4. NACA65-519 a=0.6
5. GA 37A418
6. GA 37A420
7. NACA65-519 a=0.5
8. GA 40A420
9. GA 35A418
10. GA 35A420
11. GA 40-420
12. NACA64A519
13. RONCZ 1082 VOYAGER ROOT OUTER AFT WING
14. RONCZ 1080 VOYAGER INNER AFT WING
15. GA 37-419
16. GA 37-420
17. NACA63A519
18. GA 40A418
19. NACA65-520 a=0.6
20. NACA65-520 a=0.5
21. NACA64A619