Similarly shaped airfoils to Joukowsky 15.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2015.00%25%20thick%200.00%25%20camber.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 169
3. Joukowsky 14.00% thick 0.00% camber
4. Joukowsky 16.00% thick 0.00% camber
5. GOE 410
6. FX LIII-142 K 25
7. EPPLER 474
8. EPPLER 473
9. FX 71-L-150/20
10. EPPLER 479
11. FX 71-L-150/30
12. SU-26M
13. S8035 (14%)
14. St. CYR 172 (Royer)
15. FX 71-L-150/25
16. Horten 14.00% thick 0.00% camber
17. HM50T
18. EPPLER 475
19. Horten 15.00% thick 0.00% camber
20. NACA63-015
21. GA 35-015