Similarly shaped airfoils to S8037 (16%)


New! Bulk download of polars in Excel format: s8037.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
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. S8036 (16%)
2. GEMINI (smoothed)
3. GA 35A316
4. TsAGI B 15.5% thick
5. GA 37A316
6. GA 35A216
7. NACA64-517 a=0.0
8. NACA64-417 a=0.2
9. NACA65-416 a=0.2
10. TsAGI B 15.0% thick
11. NACA64-416 a=0.2
12. GA 35A317
13. GA 37A216
14. TsAGI B 16.0% thick
15. NACA64-516 a=0.0
16. GA 30-316
17. GA 30A316
18. NACA65-516 a=0.0
19. NACA65-416 a=0.0
20. NACA65-417 a=0.2
21. NACA63-417 a=0.2