Similarly shaped airfoils to Horten 17.00% thick 1.00% camber


New! Bulk download of polars in Excel format: Horten%2017.00%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

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1. NACA23017
2. NACA23016.5
3. NACA23017.424
4. Horten 18.00% thick 1.00% camber
5. Horten 16.00% thick 1.00% camber
6. Horten 17.00% thick 0.00% camber
7. NACA23117
8. NACA0017
9. GA 30-017
10. NACA22016
11. NACA23116.5
12. GA 30A017
13. NACA24017
14. NACA23016
15. NACA24016.5
16. GA 30-016
17. NACA23015.9
18. NACA23018
19. GA 30A016
20. NACA22016.5
21. NACA0016