Similarly shaped airfoils to GA 30A018
New! Bulk download of polars in Excel format: GA%2030A018.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 30-018
3. Horten 18.00% thick 0.00% camber
4. Horten 19.00% thick 0.00% camber
5. GA 30A019
6. GA 30A017
7. GA 30-019
8. GA 30-017
9. Horten 18.00% thick 1.00% camber
10. NACA0017
11. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
12. GA 35A018
13. GA 35A019
14. NACA63A018
15. Horten 19.00% thick 1.00% camber
16. Horten 17.00% thick 0.00% camber
17. TRAINER60
18. GA 37A018
19. GA 37A019
20. NACA63A119
21. NACA23018