Similarly shaped airfoils to GA 30-018


New! Bulk download of polars in Excel format: GA%2030-018.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. NACA0018
2. GA 30A018
3. Horten 18.00% thick 0.00% camber
4. Horten 19.00% thick 0.00% camber
5. GA 30-019
6. GA 30-017
7. GA 30A017
8. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
9. Horten 18.00% thick 1.00% camber
10. GA 30A019
11. NACA0017
12. GA 35A018
13. NACA63A018
14. GA 35A019
15. Horten 17.00% thick 0.00% camber
16. Horten 19.00% thick 1.00% camber
17. TRAINER60
18. GA 35-019
19. GA 37-019
20. GA 37A018
21. GA 37A019