Similarly shaped airfoils to Horten 11.00% thick 1.00% camber


New! Bulk download of polars in Excel format: Horten%2011.00%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. HM391-1
2. NACA22010.5
3. MJZ1211
4. NPL 9660
5. NPL 9615
6. JWL081 11/1.3
7. Horten 10.00% thick 1.00% camber
8. Ritz 1-30-12
9. NACA22110.5
10. HM391-2
11. GIII BL45
12. MH 108 11.98%
13. NACA23110.5
14. NACA63-211 a=0.0
15. NACA63-111 a=0.2
16. NACA23010.5
17. NACA63-111 a=0.5
18. NACA63-111 a=0.0
19. NACA22010
20. Horten 11.00% thick 2.00% camber
21. ONERA NACA CAMBRE