Similarly shaped airfoils to NACA0018
New! Bulk download of polars in Excel format: NACA0018.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (28) | 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 30A018
3. Horten 18.00% thick 0.00% camber
4. GA 30A017
5. GA 30-017
6. Horten 19.00% thick 0.00% camber
7. NACA0017
8. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
9. Horten 18.00% thick 1.00% camber
10. Horten 17.00% thick 0.00% camber
11. GA 30-019
12. GA 30A019
13. GA 35A018
14. NACA63A018
15. TRAINER60
16. GA 35A019
17. Horten 19.00% thick 1.00% camber
18. Horten 17.00% thick 1.00% camber
19. GA 37A018
20. GA 35-019
21. NACA63A118