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
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. 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