Similarly shaped airfoils to GA 40-313
New! Bulk download of polars in Excel format: GA%2040-313.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. NACA65-413 a=0.5
3. GA 37A313
4. NACA65-413 a=0.6
5. GA 35A313
6. GA 37-313
7. NACA64-413 a=0.5
8. NACA64-413 a=0.6
9. NACA65-413 a=0.8
10. NACA65-413 a=0.2
11. NACA65-513
12. NACA65-513 a=0.0
13. GA 40A312
14. NACA64A413
15. GA 40-312
16. GA 40-314
17. GA 40A314
18. GA 37A312
19. EPPLER 231
20. NACA65-412 a=0.5
21. GA 37-314