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
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 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