Similarly shaped airfoils to JWL066 8.7/1.9


New! Bulk download of polars in Excel format: JWL066.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. NACA25009
2. PW106
3. JWL075 8.8/1.76
4. PW106 sm
5. GIII BL430
6. NACA2209
7. GIII BL450
8. NACA24009
9. BOEING-VERTOL VR-14
10. EPPLER 221
11. PW98 sm
12. HS 522
13. B-29 TIP
14. MH 20 9.01%
15. NACA M11
16. PW98-mod sm
17. NACA25109
18. MH 42 8.94%
19. NACA M11 (NACA-TR-221)
20. NACA M5
21. NACA23008