Similarly shaped airfoils to GOE 244 (MVA PR.4)


New! Bulk download of polars in Excel format: goe244.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 523
2. GOE 525
3. Joukowsky 17.00% thick 10.00% camber
4. Joukowsky 16.00% thick 10.00% camber
5. Joukowsky 18.00% thick 10.00% camber
6. EPPLER 420
7. Joukowsky 15.00% thick 10.00% camber
8. Joukowsky 19.00% thick 10.00% camber
9. GOE 241 (MVA PR.1)
10. GOE 482
11. FX 72-MS-150B
12. GOE 440
13. GOE 243 (MVA PR.3)
14. Joukowsky 14.00% thick 10.00% camber
15. ISHAAN_001
16. Joukowsky 20.00% thick 10.00% camber
17. FX 74_CL5_140
18. Joukowsky 17.00% thick 9.00% camber
19. Joukowsky 16.00% thick 9.00% camber
20. Joukowsky 18.00% thick 9.00% camber
21. CH10 (smoothed)