Similarly shaped airfoils to S9104BTE


New! Bulk download of polars in Excel format: s9104BTE.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
Dynamic plotter New!
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.

1. S9104
2. GOE 531
3. BE183-176 (inverted)
4. GOE 462
5. ISHAAN_001
6. Joukowsky 9.00% thick 10.00% camber
7. EPPLER 420
8. Joukowsky 10.00% thick 10.00% camber
9. CH10 (smoothed)
10. FX 74-Cl5-140 MOD (smoothed)
11. Joukowsky 11.00% thick 10.00% camber
12. Joukowsky 12.00% thick 10.00% camber
13. BE6699 (6.6% max t/c 9.9% max camber) CLmax 2.1 at RE 100000 transition free
14. GOE 525
15. GOE 523
16. Joukowsky 13.00% thick 10.00% camber
17. EPPLER 423
18. FX 74_CL5_140
19. GOE 448
20. GOE 244 (MVA PR.4)
21. Joukowsky 14.00% thick 10.00% camber