Similarly shaped airfoils to GA 35A310
New! Bulk download of polars in Excel format: GA%2035A310.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 40A310
3. GA 40-310
4. GA 37-310
5. NACA64-410 a=0.5
6. GA 30-310
7. GA 35-310
8. GA 30A310
9. NACA63-410 a=0.5
10. NACA64-410 a=0.6
11. NACA65-410 a=0.5
12. SD7084 (9.6%)
13. FX 84-W-097
14. EPPLER EB380
15. NACA63-410 a=0.6
16. NACA65-410 a=0.6
17. NACA63A410
18. NACA64-410 a=0.2
19. GA 37-311
20. S3014-095-85
21. DP2.47/9.48_DS