Similarly shaped airfoils to GA 35-310
New! Bulk download of polars in Excel format: GA%2035-310.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA63-410 a=0.5
3. FX 84-W-097
4. NACA63-410 a=0.6
5. NACA64-410 a=0.5
6. GA 35A310
7. S3014-095-85
8. NACA64-410 a=0.6
9. NACA63-410 a=0.2
10. SD7084 (9.6%)
11. GA 37A310
12. GA 40-310
13. NACA64-410 a=0.2
14. GA 40A310
15. EPPLER EB380
16. NACA63-410 a=0.8
17. S3016-095-87
18. MH 117 9.8%
19. GA 30-310
20. HQ 2.5/10
21. SD8040 (10%)