Similarly shaped airfoils to GOE 448
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. FX 74-Cl5-140 MOD (smoothed)
8. USA 31
9. Joukowsky 14.00% thick 10.00% camber
10. Joukowsky 13.00% thick 10.00% camber
11. Joukowsky 15.00% thick 10.00% camber
12. USA 32
13. GOE 523
14. GOE 525
15. Joukowsky 12.00% thick 10.00% camber
16. Joukowsky 16.00% thick 10.00% camber
17. GOE 482
18. GOE 244 (MVA PR.4)
19. Joukowsky 11.00% thick 10.00% camber
20. Joukowsky 17.00% thick 10.00% camber
21. Joukowsky 14.00% thick 9.00% camber