Similarly shaped airfoils to EPPLER 377MOD
New! Bulk download of polars in Excel format: e377m.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. EPPLER 377
3. EPPLER 379
4. EPPLER 378
5. Jedeslsky EJ85
6. GOE 464
7. MID 110
8. MID 111
9. GOE 803 (HACKLINGER)
10. MID 112
11. GOE 417A (GEW. PLATTE)
12. GOE 395
13. NACA M25
14. M 77
15. MID 122
16. M 7372
17. GOE 265
18. GOE 342
19. BE6568 6.5% t/c 7.5% camber Suitable for F1A towline glider category
20. MID 115
21. BE6699 (6.6% max t/c 9.9% max camber) CLmax 2.1 at RE 100000 transition free