Similarly shaped airfoils to GA 37A315
New! Bulk download of polars in Excel format: GA%2037A315.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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 40A315
3. MB253515 15.0% smoothed
4. GA 40-315
5. NACA65-415 a=0.5
6. NACA65-415 a=0.6
7. AVISTAR
8. NACA64A415
9. NACA63A415
10. GA 37-315
11. GA 37A316
12. GA 37A314
13. GA 40A316
14. NACA65-415 a=0.8
15. NACA64-415 a=0.5
16. NACA64-415 a=0.6
17. GA 35A314
18. NACA65-515
19. GA 40-316
20. GA 35A316
21. NACA65(2)-415 a=0.5