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
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
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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