Similarly shaped airfoils to Horten 10.00% thick 1.00% camber
New! Bulk download of polars in Excel format: Horten%2010.00%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
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. NACA22010
3. Ritz 1-30-10
4. HM391-2
5. EPPLER 226
6. NACA22110
7. NACA22010.5
8. GIII BL86
9. GIII BL75
10. NACA1410
11. Horten 11.00% thick 1.00% camber
12. Horten 9.00% thick 1.00% camber
13. RS001m05
14. NACA63-110 a=0.2
15. RS001m60
16. NACA63-210 a=0.0
17. NACA23010
18. NACA63-110 a=0.0
19. NACA22110.5
20. NACA63-110 a=0.5
21. EH 1.0/9.0