Similarly shaped airfoils to Horten 19.00% thick 1.00% camber


New! Bulk download of polars in Excel format: Horten%2019.00%25%20thick%201.00%25%20camber.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. NACA23018.87
2. NACA23019
3. Horten 20.00% thick 1.00% camber
4. Horten 18.00% thick 1.00% camber
5. Horten 19.00% thick 2.00% camber
6. Horten 19.00% thick 0.00% camber
7. GA 30-019
8. NACA24019
9. GA 30A019
10. NACA23018
11. GA 30-018
12. GA 30A018
13. NACA25019
14. NACA0018
15. Horten 20.00% thick 0.00% camber
16. NACA23118
17. Horten 20.00% thick 2.00% camber
18. Horten 18.00% thick 0.00% camber
19. NACA2219
20. NACA24018
21. NACA23119