Similarly shaped airfoils to GA 40-315
New! Bulk download of polars in Excel format: GA%2040-315.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. NACA65-415 a=0.5
3. NACA65-415 a=0.6
4. GA 37A315
5. GA 35A315
6. NACA65-415 a=0.8
7. GA 37-315
8. MB253515 15.0% smoothed
9. NACA65-515
10. NACA65(2)-415 a=0.5
11. NACA65(2)-415
12. NACA64-415 a=0.5
13. NACA64-415 a=0.6
14. GA 40-316
15. GA 40A314
16. GA 40-314
17. NACA65-515 a=0.0
18. GA 40A316
19. NACA65-415 a=0.2
20. FX 79-K-144/17
21. NACA64A415