Similarly shaped airfoils to FX 73-CL2-152
New! Bulk download of polars in Excel format: fx73cl2152.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. Joukowsky 14.00% thick 7.00% camber
3. Joukowsky 15.00% thick 7.00% camber
4. GOE 227 (MVA H.37)
5. Joukowsky 15.00% thick 8.00% camber
6. Joukowsky 14.00% thick 8.00% camber
7. Joukowsky 13.00% thick 7.00% camber
8. USA 98
9. MH 113 14.62%
10. GOE 242 (MVA PR.2)
11. Joukowsky 16.00% thick 7.00% camber
12. FX 63-137
13. MH 114 13.02%
14. GOE 225 (MVA H.35)
15. GOE 501
16. Joukowsky 16.00% thick 8.00% camber
17. Joukowsky 13.00% thick 8.00% camber
18. GOE 226 (MVA H.36)
19. FX 73-CL3-152
20. GOE 441
21. GOE 535