Similarly shaped airfoils to GOE 242 (MVA PR.2)


New! Bulk download of polars in Excel format: goe242.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
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 8.00% camber
3. Joukowsky 16.00% thick 8.00% camber
4. GOE 441
5. EPPLER 591
6. Joukowsky 14.00% thick 8.00% camber
7. FX 72-MS-150A
8. FX 73-CL3-152
9. GOE 226 (MVA H.36)
10. MH 113 14.62%
11. FX 73-CL2-152
12. Joukowsky 17.00% thick 8.00% camber
13. Joukowsky 15.00% thick 9.00% camber
14. Joukowsky 16.00% thick 9.00% camber
15. MH 112 16.2%
16. Joukowsky 15.00% thick 7.00% camber
17. Joukowsky 13.00% thick 8.00% camber
18. Joukowsky 14.00% thick 9.00% camber
19. Joukowsky 16.00% thick 7.00% camber
20. GOE 225 (MVA H.35)
21. Joukowsky 17.00% thick 9.00% camber