Similarly shaped airfoils to NACA M13 (NACA-TR-221)
New! Bulk download of polars in Excel format: NACA%20M13%20%28NACA-TR-221%29.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
Dynamic plotter New!
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. NACA M16 (NACA-TR-221)
3. GOE 590
4. NACA M13
5. NACA35007
6. GOE 235
7. GOE 113
8. NACA45007
9. I.S.A. 571
10. GOE 587
11. Coanda 1
12. GOE 419
13. NACA44007
14. NACA M7 (NACA-TR-221)
15. GOE 346 (FRIEDRICHSHAFEN-STAAKEN)
16. GOE 377
17. GOE 100 (SOPWITH)
18. GOE 142 (MVA H.19)
19. BE50 (original)
20. GOE 488
21. GOE 393