Similarly shaped airfoils to DAE-31


New! Bulk download of polars in Excel format: dae31.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (3) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
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.

1. DAE-21
2. GOE 405
3. MID 405e
4. MID 405w2
5. GOE 332 (PFALZ 61)
6. Joukowsky 12.00% thick 7.00% camber
7. GOE 239 (MVA H.31)
8. DAE-11
9. AH 79-100 C
10. GOE 301 (FRIEDRICHSHAFEN G 13)
11. GOE 501
12. Joukowsky 11.00% thick 7.00% camber
13. GOE 801 (MVA 301)
14. GOE 802
15. GOE 331 (PFALZ 60)
16. MH 114 13.02%
17. GOE 528
18. AH 79-100 B
19. MH 115 11.06%
20. Joukowsky 13.00% thick 7.00% camber
21. GOE 431