Similarly shaped airfoils to NACA23110.5
New! Bulk download of polars in Excel format: NACA23110.5.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. NACA22110.5
3. HM391-2
4. NACA22010.5
5. NACA22110
6. NACA23110
7. NACA22010
8. NACA23010.5
9. HM391-1
10. NACA23010
11. Horten 11.00% thick 2.00% camber
12. Horten 11.00% thick 1.00% camber
13. Horten 10.00% thick 1.00% camber
14. Horten 10.00% thick 2.00% camber
15. NACA32010.5
16. LOCKHEED-GEORGIA SUPERCRITICAL
17. NACA32110
18. EPPLER 186
19. NACA24110.5
20. GIII BL45
21. GIII BL75