Similarly shaped airfoils to FX 73-CL3-152
New! Bulk download of polars in Excel format: fx73cl3152.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
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. EPPLER 421
3. GOE 441
4. GOE 227 (MVA H.37)
5. Joukowsky 14.00% thick 8.00% camber
6. Joukowsky 15.00% thick 8.00% camber
7. Joukowsky 15.00% thick 9.00% camber
8. Joukowsky 14.00% thick 9.00% camber
9. GOE 242 (MVA PR.2)
10. GOE 225 (MVA H.35)
11. Joukowsky 13.00% thick 8.00% camber
12. FX 72-MS-150A
13. GOE 482
14. Joukowsky 16.00% thick 9.00% camber
15. Joukowsky 16.00% thick 8.00% camber
16. Joukowsky 13.00% thick 9.00% camber
17. FX 73-CL2-152
18. MH 113 14.62%
19. EPPLER 591
20. GOE 630
21. Joukowsky 12.00% thick 8.00% camber