Similarly shaped airfoils to MID 405e
New! Bulk download of polars in Excel format: MID%20405e.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. DAE-21
3. DAE-11
4. DAE-31
5. GOE 501
6. Joukowsky 13.00% thick 7.00% camber
7. Joukowsky 12.00% thick 7.00% camber
8. MH 114 13.02%
9. GOE 405
10. GOE 528
11. FX 74-CL6-140
12. EPPLER 422
13. Joukowsky 14.00% thick 7.00% camber
14. GOE 332 (PFALZ 61)
15. Joukowsky 11.00% thick 7.00% camber
16. GOE 239 (MVA H.31)
17. GOE 630
18. GOE 431
19. Joukowsky 13.00% thick 6.00% camber
20. Joukowsky 12.00% thick 6.00% camber
21. FX 63-137