Similarly shaped airfoils to GA 35A317
New! Bulk download of polars in Excel format: GA%2035A317.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 40A317
3. NACA63A417
4. GA 40-317
5. GA 37-317
6. NACA64A417
7. GA 37-318
8. GA 35A316
9. GA 35A318
10. NACA65-417 a=0.5
11. NACA65-417 a=0.6
12. GOE 601
13. GA 37A318
14. GA 37A316
15. NACA64-417 a=0.6
16. NACA64-417 a=0.5
17. GA 30-317
18. GA 35-317
19. NACA64-418 a=0.6
20. GA 30-316
21. NACA64-418 a=0.5