Similarly shaped airfoils to FAD04


New! Bulk download of polars in Excel format: FAD04.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. MH 61 10.26%
2. HM50
3. AZcombat1
4. MH 45 9.85%
5. MH 60 10.08%
6. HM10011
7. BOEING-VERTOL V23010-1.58
8. MH 44 9.66%
9. JWL081 11/1.3
10. Horten 10.00% thick 2.00% camber
11. EH 2.0/10
12. Joukowsky 11.00% thick 1.00% camber
13. NACA63-210 a=0.2
14. HM391-2
15. HM55
16. RS001m05
17. HM56
18. RS001
19. NACA63-210 a=0.0
20. NACA23010
21. Horten 10.00% thick 1.00% camber