Similarly shaped airfoils to GOE 614
New! Bulk download of polars in Excel format: goe614.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. USA 35 A
3. GOE 620
4. GOE 422
5. GOE 229 (MVA H.39)
6. GOE 223 (MVA H.34)
7. GOE 289 (MVA 289)
8. RONCZ 1046 VOYAGER CANARD
9. GOE 625
10. GOE 504
11. GOE 384
12. EPPLER 857
13. FX 76-MP-160
14. GOE 527
15. GOE 288
16. GOE 449
17. GOE 382
18. GOE 508
19. Joukowsky 19.00% thick 7.00% camber
20. GOE 514
21. Joukowsky 20.00% thick 7.00% camber