Similarly shaped airfoils to GOE 482
New! Bulk download of polars in Excel format: goe482.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 16.00% thick 9.00% camber
3. GOE 241 (MVA PR.1)
4. EPPLER 421
5. Joukowsky 17.00% thick 9.00% camber
6. FX 73-CL3-152
7. Joukowsky 15.00% thick 9.00% camber
8. FX 72-MS-150A
9. USA 31
10. Joukowsky 16.00% thick 10.00% camber
11. Joukowsky 17.00% thick 10.00% camber
12. Joukowsky 18.00% thick 9.00% camber
13. JN-153
14. MH 112 16.2%
15. FX 72-MS-150B
16. Joukowsky 15.00% thick 10.00% camber
17. Joukowsky 18.00% thick 10.00% camber
18. GOE 243 (MVA PR.3)
19. GOE 440
20. FX 72-LS-160
21. GOE 242 (MVA PR.2)