Similarly shaped airfoils to Joukowsky 14.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2014.00%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. Joukowsky 13.00% thick 0.00% camber
3. Joukowsky 15.00% thick 0.00% camber
4. HM50T
5. FX LIII-142 K 25
6. EPPLER 474
7. St. CYR 172 (Royer)
8. Horten 13.00% thick 0.00% camber
9. EPPLER 168
10. S8035 (14%)
11. FX 71-120
12. EPPLER 478
13. GA 30-013
14. Horten 14.00% thick 0.00% camber
15. GA 35-014
16. NACA0013
17. FX 71-L-150/20
18. BOEING 737 MIDSPAN
19. GA 35-013
20. RAF 30
21. EPPLER EA 6(-1)-012