Similarly shaped airfoils to NACA M27
New! Bulk download of polars in Excel format: m27.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
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2. GOE 573
3. GOE 320 (HANSA-BRANDENBURG II.1)
4. GOE 366
5. GOE 14
6. GOE 364
7. GOE 630
8. GOE 15
9. GOE 322 (HANSA-BRANDENBURG IV.1)
10. NACA M24
11. EPPLER 422
12. GOE 562
13. CHEN
14. NACA M26
15. GOE 744
16. NACA M21
17. Horten 11.00% thick 10.00% camber
18. GOE 528
19. GOE 332 (PFALZ 61)
20. GOE 405
21. Horten 12.00% thick 9.00% camber