Similarly shaped airfoils to GOE 288
New! Bulk download of polars in Excel format: goe288.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. GOE 498
3. GOE 289 (MVA 289)
4. GOE 647
5. EPPLER 561
6. GOE 620
7. Joukowsky 18.00% thick 6.00% camber
8. Joukowsky 17.00% thick 6.00% camber
9. GOE 527
10. GOE 508
11. GOE 433
12. GOE 624
13. GOE 502
14. GOE 223 (MVA H.34)
15. GOE 612
16. GOE 621
17. GOE 481A
18. GOE 413
19. Joukowsky 19.00% thick 6.00% camber
20. DOUGLAS LA203A
21. GOE 675