Similarly shaped airfoils to GA 37A213
New! Bulk download of polars in Excel format: GA%2037A213.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. GA 40A213
3. GA 40-213
4. NACA65-313 a=0.5
5. NACA64A313
6. NACA63A313
7. NACA65-313 a=0.6
8. NACA65-313 a=0.2
9. GA 37-213
10. NACA64-313 a=0.5
11. NACA65-313 a=0.8
12. GOE 600
13. NACA65-313
14. NACA64-313 a=0.6
15. NACA65-313 a=0.0
16. S8055 (12%)
17. NACA64-313 a=0.2
18. GA 37A212
19. GA 40A214
20. GA 37A214
21. NACA65A313