Similarly shaped airfoils to GOE 448
New! Bulk download of polars in Excel format: goe448.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. EPPLER 423
3. CH10 (smoothed)
4. GOE 440
5. FX 74_CL5_140
6. FX 72-MS-150B
7. ISHAAN_001
8. FX 74-Cl5-140 MOD (smoothed)
9. USA 31
10. Joukowsky 14.00% thick 10.00% camber
11. Joukowsky 13.00% thick 10.00% camber
12. Joukowsky 15.00% thick 10.00% camber
13. USA 32
14. GOE 525
15. GOE 523
16. Joukowsky 12.00% thick 10.00% camber
17. Joukowsky 16.00% thick 10.00% camber
18. GOE 482
19. GOE 244 (MVA PR.4)
20. Joukowsky 11.00% thick 10.00% camber
21. Joukowsky 17.00% thick 10.00% camber