Similarly shaped airfoils to Horten 11.00% thick 1.00% camber
New! Bulk download of polars in Excel format: Horten%2011.00%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. NACA22010.5
3. MJZ1211
4. NPL 9660
5. NPL 9615
6. JWL081 11/1.3
7. Horten 10.00% thick 1.00% camber
8. Ritz 1-30-12
9. NACA22110.5
10. HM391-2
11. GIII BL45
12. MH 108 11.98%
13. NACA23110.5
14. NACA63-211 a=0.0
15. NACA63-111 a=0.2
16. NACA23010.5
17. NACA63-111 a=0.5
18. NACA63-111 a=0.0
19. NACA22010
20. Horten 11.00% thick 2.00% camber
21. ONERA NACA CAMBRE