Similarly shaped airfoils to Horten 9.00% thick 2.00% camber


New! Bulk download of polars in Excel format: Horten%209.00%25%20thick%202.00%25%20camber.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. EH 1.5/9.0
2. BW 05 02 09
3. PW51
4. PW75
5. PW75 sm
6. NACA23109
7. JWL068 9.5/1.7
8. NACA24109
9. NACA23009
10. NACA24009
11. AZ2004_9
12. PW51 sm
13. PW98 sm
14. CJ3209
15. NACA25009
16. TsAGI B 9.0% thick
17. TsAGI B 8.5% thick
18. BOEING VERTOL V(1.95)3009-1.25
19. Horten 10.00% thick 2.00% camber
20. AZ2005tip
21. JWL075 8.8/1.76