Similarly shaped airfoils to GA 30A017
New! Bulk download of polars in Excel format: GA%2030A017.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
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.
2. GA 30-017
3. Horten 17.00% thick 0.00% camber
4. NACA0018
5. Horten 18.00% thick 0.00% camber
6. GA 30A016
7. GA 30A018
8. GA 30-018
9. GA 30-016
10. Horten 17.00% thick 1.00% camber
11. NACA0016
12. GA 35A017
13. NACA63A017
14. GA 35A018
15. EPPLER 476
16. NACA63A018
17. Horten 16.00% thick 0.00% camber
18. Horten 18.00% thick 1.00% camber
19. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
20. TRAINER60
21. GA 37A017