Similarly shaped airfoils to GA 30-017


New! Bulk download of polars in Excel format: GA%2030-017.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. NACA0017
2. GA 30A017
3. Horten 17.00% thick 0.00% camber
4. Horten 18.00% thick 0.00% camber
5. NACA0018
6. GA 30-016
7. GA 30-018
8. GA 30A016
9. EPPLER 476
10. Horten 17.00% thick 1.00% camber
11. GA 30A018
12. GA 35A017
13. NACA63A017
14. NACA0016
15. NACA63A018
16. GA 35A018
17. Horten 16.00% thick 0.00% camber
18. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
19. TRAINER60
20. Horten 18.00% thick 1.00% camber
21. GA 35-018