Similarly shaped airfoils to GA 37A418
New! Bulk download of polars in Excel format: GA%2037A418.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 40A418
3. GA 40-418
4. RONCZ 1082 VOYAGER ROOT OUTER AFT WING
5. RONCZ 1080 VOYAGER INNER AFT WING
6. NACA65-518 a=0.6
7. NACA65-518 a=0.5
8. GA 37A419
9. GA 37A417
10. GA 40A419
11. GA 35A417
12. GA 35A419
13. GA 40-419
14. NACA64A518
15. GA 37-418
16. GA 37-419
17. NACA63A518
18. NACA65-519 a=0.6
19. GA 40A417
20. NACA65-519 a=0.5
21. NACA65-518 a=0.8