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