Similarly shaped airfoils to ZAGI 10
New! Bulk download of polars in Excel format: ZAGI%2010.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. Sipkill 1.7/10
3. TsAGI B 9.5% thick
4. TsAGI B 10.5% thick
5. NACA25010
6. FX 69-H-098
7. NACA25010.5
8. RC-10(N)1
9. NACA24010
10. RC-10(B)3
11. EH 2.0/10
12. NACA 5-H-10
13. NACA24010.5
14. RC_Milan
15. NACA25110
16. NACA2210
17. RC(5)-10
18. NACA65-310 a=0.0
19. BOEING-VERTOL VR-13
20. BOEING 737 MIDSPAN
21. NACA25110.5