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
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. 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