Similarly shaped airfoils to NACA M27 (NACA-TR-221)
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
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
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2. GOE 331 (PFALZ 60)
3. GOE 630
4. GOE 366
5. NACA M24 (NACA-TR-221)
6. GOE 15
7. GOE 320 (HANSA-BRANDENBURG II.1)
8. GOE 364
9. GOE 14
10. GOE 573
11. EPPLER 422
12. GOE 562
13. GOE 322 (HANSA-BRANDENBURG IV.1)
14. FX 74-CL6-140
15. GOE 332 (PFALZ 61)
16. NACA M26 (NACA-TR-221)
17. GOE 405
18. NACA M26
19. GOE 447
20. GOE 528
21. DAE-11