Similarly shaped airfoils to MID 405w2
New! Bulk download of polars in Excel format: MID%20405w2.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-11
3. DAE-21
4. MH 114 13.02%
5. DAE-31
6. GOE 501
7. GOE 332 (PFALZ 61)
8. GOE 405
9. GOE 446
10. GOE 528
11. EPPLER 422
12. Joukowsky 13.00% thick 7.00% camber
13. Joukowsky 14.00% thick 7.00% camber
14. GOE 630
15. FX 74-CL6-140
16. Joukowsky 12.00% thick 7.00% camber
17. FX 76-MP-120
18. FX 76-MP-140
19. GOE 366
20. FX 63-137
21. MID 406w2