Similarly shaped airfoils to GA 30-015


New! Bulk download of polars in Excel format: GA%2030-015.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. NACA0015
2. GA 30A015
3. Horten 15.00% thick 0.00% camber
4. EPPLER 477
5. Horten 16.00% thick 0.00% camber
6. NACA0016
7. EPPLER 475
8. GA 35A015
9. NACA63-015A
10. NACA63A015
11. GA 30-016
12. GA 30-014
13. GA 30A014
14. GA 30A016
15. GA 35A016
16. NACA63A016
17. Horten 15.00% thick 1.00% camber
18. GA 35-016
19. Horten 14.00% thick 0.00% camber
20. GA 37A015
21. NACA64(2)-015A