Similarly shaped airfoils to PW51


New! Bulk download of polars in Excel format: PW51.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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. PW75
2. PW75 sm
3. AZ2004_9
4. PW51 sm
5. EH 1.5/9.0
6. AZ2005tip
7. salaztip
8. AZ2005mid
9. Horten 9.00% thick 2.00% camber
10. TL56
11. NACA23009
12. JWL068 9.5/1.7
13. JWL074 8.5/1.2
14. PW98 sm
15. NACA23109
16. PW Rennbrett Strak 1 final Mod
17. BOEING VERTOL V(1.95)3009-1.25
18. MH 46 9.1%
19. JWL078 8/1
20. NACA22009
21. PW98-mod sm