Similarly shaped airfoils to SG6041_CMPLXFOIL
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. GOE 500
3. AH 79-100 C
4. Joukowsky 11.00% thick 6.00% camber
5. Joukowsky 12.00% thick 6.00% camber
6. MH 115 11.06%
7. EPPLER 216
8. Joukowsky 10.00% thick 6.00% camber
9. NACA6410
10. GOE 239 (MVA H.31)
11. EPPLER 395
12. GOE 501
13. AH 79-100 B
14. Joukowsky 11.00% thick 7.00% camber
15. Joukowsky 12.00% thick 7.00% camber
16. GOE 190 (MVA MK.18)
17. Joukowsky 13.00% thick 6.00% camber
18. AF104k
19. FX 63-120
20. GOE 497
21. GOE 358