Similarly shaped airfoils to Horten 12.00% thick 1.00% camber
New! Bulk download of polars in Excel format: Horten%2012.00%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. NACA22112
3. NPL 9626
4. MJZ1211
5. MH 106 13.07%
6. NACA23012
7. Horten 13.00% thick 1.00% camber
8. BOEING 737 MIDSPAN
9. NACA23112
10. NACA63-112 a=0.0
11. Horten 12.00% thick 0.00% camber
12. NACA63-112 a=0.2
13. NPL 9627
14. NACA0012
15. GA 30-012
16. MH 108 11.98%
17. FX 76-120
18. NACA63-113 a=0.0
19. GA 30A012
20. Horten 11.00% thick 1.00% camber
21. NACA63-113 a=0.2