Similarly shaped airfoils to EPPLER 417
New! Bulk download of polars in Excel format: e417.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. NLF(2)-0415
3. DFVLR R-4
4. SOMERS S102 (BLUNT)
5. LS(1)-0413 (GA(W)-2)
6. NACA65(2)-415
7. NACA65-414
8. NACA65-514
9. NACA64A414
10. NACA64(2)-415
11. NACA65-415
12. NACA65-515
13. NACA63A414
14. NACA65-414 a=0.8
15. LOCKHEED L-188 ROOT
16. NACA65A414
17. MH 200 12.97%
18. NACA64-515
19. NACA65-314 a=0.8
20. NACA65-415 a=0.8
21. NACA64A415