Similarly shaped airfoils to GA 30-016


New! Bulk download of polars in Excel format: GA%2030-016.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. NACA0016
2. GA 30A016
3. Horten 16.00% thick 0.00% camber
4. Horten 17.00% thick 0.00% camber
5. EPPLER 476
6. NACA0017
7. GA 30-015
8. GA 30-017
9. GA 30A015
10. GA 35A016
11. NACA63A016
12. GA 30A017
13. Horten 16.00% thick 1.00% camber
14. NACA0015
15. GA 35A017
16. NACA63A017
17. Horten 15.00% thick 0.00% camber
18. GA 35-017
19. EPPLER 477
20. NACA22016
21. GA 37-017