Similarly shaped airfoils to S9104
New! Bulk download of polars in Excel format: s9104.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. GOE 531
3. GOE 462
4. Joukowsky 9.00% thick 10.00% camber
5. Joukowsky 10.00% thick 10.00% camber
6. EPPLER 420
7. CH10 (smoothed)
8. FX 74-Cl5-140 MOD (smoothed)
9. Joukowsky 11.00% thick 10.00% camber
10. Joukowsky 12.00% thick 10.00% camber
11. BE6699 (6.6% max t/c 9.9% max camber) CLmax 2.1 at RE 100000 transition free
12. GOE 523
13. GOE 525
14. Joukowsky 13.00% thick 10.00% camber
15. EPPLER 423
16. FX 74_CL5_140
17. GOE 448
18. GOE 244 (MVA PR.4)
19. Joukowsky 14.00% thick 10.00% camber
20. RAF 19
21. S1223