Similarly shaped airfoils to Horten 9.00% thick 1.00% camber
New! Bulk download of polars in Excel format: Horten%209.00%25%20thick%201.00%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. NACA22009
3. EH 1.5/9.0
4. NACA22109
5. BOEING VERTOL V(1.95)3009-1.25
6. JWL074 8.5/1.2
7. NACA63-109 a=0.2
8. NACA1409
9. SIKORSKY SC1095
10. Horten 10.00% thick 1.00% camber
11. PW51
12. PW75
13. PW75 sm
14. NACA63-109 a=0.0
15. AZ2005tip
16. SC17
17. NACA63-209 a=0.0
18. NACA63-109 a=0.5
19. RS001m05
20. PW51 sm
21. AZ2004_9