Similarly shaped airfoils to GOE 229 (MVA H.39)
New! Bulk download of polars in Excel format: goe229.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 614
3. GOE 620
4. EPPLER 857
5. Joukowsky 19.00% thick 6.00% camber
6. Joukowsky 19.00% thick 7.00% camber
7. Joukowsky 20.00% thick 7.00% camber
8. Joukowsky 20.00% thick 6.00% camber
9. Joukowsky 18.00% thick 6.00% camber
10. FX 76-MP-160
11. GOE 222 (MVA H.33)
12. Joukowsky 18.00% thick 7.00% camber
13. GOE 288
14. GOE 289 (MVA 289)
15. USA 35 A
16. USA 35
17. GOE 504
18. GOE 422
19. GOE 228 (MVA H.38)
20. RONCZ 1046 VOYAGER CANARD
21. Joukowsky 17.00% thick 6.00% camber