Similarly shaped airfoils to GOE 497
New! Bulk download of polars in Excel format: goe497.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. Joukowsky 13.00% thick 5.00% camber
3. EPPLER 396
4. GOE 430
5. Joukowsky 13.00% thick 6.00% camber
6. RAF 32
7. Joukowsky 12.00% thick 5.00% camber
8. Joukowsky 14.00% thick 5.00% camber
9. EPPLER 397
10. Joukowsky 14.00% thick 6.00% camber
11. FX 63-120
12. Joukowsky 12.00% thick 6.00% camber
13. GOE 480
14. GOE 567
15. NM Retro 13
16. MH 115 11.06%
17. FX 63-137 13.7% smoothed
18. GOE 532
19. GOE 533
20. GOE 553
21. GOE 650