Similarly shaped airfoils to EPPLER 403
New! Bulk download of polars in Excel format: e403.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. SOMERS S102 (BLUNT)
4. NACA65(2)-415
5. NACA65-515
6. DORNIER A-5
7. NACA65-415 a=0.8
8. FX 60-157
9. NACA64A415
10. NACA64(2)-415
11. NACA63A415
12. NACA64-515
13. NACA65-516
14. EPPLER STF 863-615
15. NACA65-415
16. NACA65A415
17. NACA64-516
18. NACA64-415 a=0.8
19. NACA65-416 a=0.8
20. NACA65-514
21. EM J18 2515 DrW r0,8