Similarly shaped airfoils to GA 35A419
New! Bulk download of polars in Excel format: GA%2035A419.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
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 35A418
4. GA 35A420
5. GA 40-419
6. GA 37-419
7. GA 37-420
8. GA 37A420
9. GA 37A418
10. NACA63A519
11. NACA65-519 a=0.6
12. NACA65-519 a=0.5
13. NACA64A519
14. GA 30-418
15. GA 40A420
16. NACA63A619
17. GA 30-419
18. GA 35-419
19. GA 40-420
20. RONCZ 1082 VOYAGER ROOT OUTER AFT WING
21. GA 30A418