Similarly shaped airfoils to GOE 522
New! Bulk download of polars in Excel format: goe522.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
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2. GOE 386
3. GOE 434
4. MH 150 23.89%
5. GOE 383
6. EPPLER 857
7. GOE 798
8. GOE 625
9. GOE 382
10. GA 30-620
11. GA 30A620
12. GOE 777
13. GOE 424
14. Joukowsky 20.00% thick 6.00% camber
15. GA 30-619
16. GA 30A619
17. GOE 679
18. GOE 255 (MVA CA.6)
19. GOE 390
20. GA 35A620
21. Joukowsky 20.00% thick 5.00% camber