Similarly shaped airfoils to EPPLER 385
New! Bulk download of polars in Excel format: e385.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. GOE 610-B MOD.
3. NACA6409
4. GOE 195
5. HL73-650
6. GOE 456
7. GOE 458
8. Eiffel 36
9. Joukowsky 9.00% thick 6.00% camber
10. GOE 124 (MVA H.4)
11. GOE 428
12. GOE 439
13. GOE 450
14. GOE 174 (ALBATROS 5020)
15. GOE 359
16. Joukowsky 9.00% thick 5.00% camber
17. GOE 184 (MVA H.29)
18. GOE 176 (ALBATROS 7020)
19. GOE 610 B
20. AH-6-40-7
21. NACA63-709 a=0.6