Similarly shaped airfoils to FX 72-MS-150A


New! Bulk download of polars in Excel format: fx72150a.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. GOE 227 (MVA H.37)
2. Joukowsky 15.00% thick 9.00% camber
3. GOE 226 (MVA H.36)
4. Joukowsky 14.00% thick 9.00% camber
5. GOE 242 (MVA PR.2)
6. GOE 441
7. Joukowsky 16.00% thick 9.00% camber
8. Joukowsky 15.00% thick 8.00% camber
9. Joukowsky 14.00% thick 8.00% camber
10. FX 73-CL3-152
11. EPPLER 421
12. FX 76-MP-120
13. MH 113 14.62%
14. Joukowsky 13.00% thick 9.00% camber
15. GOE 482
16. Joukowsky 16.00% thick 8.00% camber
17. Joukowsky 13.00% thick 8.00% camber
18. FX 72-MS-150B
19. FX 76-MP-140
20. GOE 447
21. FX 72-LS-160