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