Similarly shaped airfoils to JWL067 11.5/1.7
New! Bulk download of polars in Excel format: JWL067.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. Horten 11.00% thick 2.00% camber
3. NACA24010.5
4. NACA23010.5
5. NACA24110.5
6. NACA32010.5
7. HM391-1
8. Borge-b3
9. HM50
10. EH 2.0/12
11. NACA25010.5
12. JWL081 11/1.3
13. BOEING-VERTOL V23010-1.58
14. NACA63-311 a=0.0
15. NACA42010.5
16. EH 2.0/10
17. Horten 10.00% thick 2.00% camber
18. NACA63-312 a=0.0
19. NACA24010
20. NACA23010
21. NACA23110