Similarly shaped airfoils to Joukowsky 15.00% thick 8.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2015.00%25%20thick%208.00%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 14.00% thick 8.00% camber
3. GOE 227 (MVA H.37)
4. GOE 226 (MVA H.36)
5. GOE 242 (MVA PR.2)
6. Joukowsky 13.00% thick 8.00% camber
7. Joukowsky 17.00% thick 8.00% camber
8. Joukowsky 15.00% thick 7.00% camber
9. GOE 441
10. Joukowsky 15.00% thick 9.00% camber
11. Joukowsky 14.00% thick 7.00% camber
12. MH 113 14.62%
13. Joukowsky 16.00% thick 9.00% camber
14. FX 73-CL3-152
15. EPPLER 591
16. Joukowsky 16.00% thick 7.00% camber
17. FX 73-CL2-152
18. GOE 225 (MVA H.35)
19. Joukowsky 14.00% thick 9.00% camber
20. FX 72-MS-150A
21. FX 76-MP-140