Similarly shaped airfoils to JWL081 11/1.3


New! Bulk download of polars in Excel format: JWL081.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. HM50
3. NACA23010.5
4. Horten 11.00% thick 1.00% camber
5. NACA24010.5
6. AMES A-01
7. Horten 11.00% thick 2.00% camber
8. NACA63-211 a=0.2
9. BOEING-VERTOL V23010-1.58
10. REPUBLIC S-3
11. NACA63-211 a=0.0
12. NACA1410
13. JWL067 11.5/1.7
14. HM391-2
15. LOCKHEED-GEORGIA SUPERCRITICAL
16. Ritz 1-30-10
17. NACA25010.5
18. NACA23010
19. NACA63-211 a=0.5
20. FAD04
21. HM10011