Similarly shaped airfoils to US1000ROOT (Great Planes R/C Ultra-Sport 1000)


New! Bulk download of polars in Excel format: us1000root.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
Dynamic plotter New!
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.

1. Horten 18.00% thick 0.00% camber
2. TRAINER60
3. NACA0018
4. GA 30-018
5. GA 30A018
6. GA 30-017
7. Horten 17.00% thick 0.00% camber
8. Horten 19.00% thick 0.00% camber
9. GA 35-019
10. GA 30A017
11. NACA0017
12. Horten 18.00% thick 1.00% camber
13. GA 35-018
14. NACA63(3)-018
15. NACA63-018
16. NACA63A018
17. GA 35A018
18. NACA63-119 a=0.0
19. GA 30-019
20. GA 37-019
21. Horten 19.00% thick 1.00% camber