Similarly shaped airfoils to GA 30-012


New! Bulk download of polars in Excel format: GA%2030-012.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. NACA0012
2. GA 30A012
3. Horten 12.00% thick 0.00% camber
4. FX 76-120
5. bradshaw_baseline
6. RAF 30
7. J5012 12%
8. EPPLER EA 6(-1)-012
9. NACA M3 (NACA-TR-221)
10. NACA M3
11. EPPLER 171
12. N-14
13. N-13
14. GA 35A012
15. NACA63A012
16. NACA63-012A
17. FX 71-120
18. Horten 13.00% thick 0.00% camber
19. FX 79-L-120
20. NACA0013
21. SC(2)-0012