Similarly shaped airfoils to EPPLER 603
New! Bulk download of polars in Excel format: e603.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (8) | 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. FX 66-S-196
3. NACA65-719
4. EPPLER 1098
5. DU 80-176 V1
6. EPPLER 655
7. FX 75-193
8. GA 40-419
9. FX 66-S-196 V1
10. GA 40-619
11. GA 40A419
12. NACA65-619 a=0.8
13. GA 40A619
14. RONCZ 1082 VOYAGER ROOT OUTER AFT WING
15. FX S 02-196
16. HQ 3.5/18
17. NACA65-619 a=0.6
18. NACA65-720
19. NACA65-619 a=0.5
20. NACA65-718
21. GA 37A419