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
Dynamic plotter New!
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.
1. GA 35A315
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