Similarly shaped airfoils to GA 35A315
New! Bulk download of polars in Excel format: GA%2035A315.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. MB253515 15.0% smoothed
3. GA 40A315
4. AVISTAR
5. GA 40-315
6. GA 37-315
7. NACA63A415
8. NACA65-415 a=0.5
9. NACA64-415 a=0.5
10. NACA64-415 a=0.6
11. NACA64A415
12. NACA65-415 a=0.6
13. GA 37-316
14. CB2515
15. GA 35A316
16. GA 35A314
17. GA 30-315
18. GA 35-315
19. GEMINI (smoothed)
20. GA 37A316
21. NACA64-416 a=0.5