Similarly shaped airfoils to Joukowsky 10.00% thick 4.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2010.00%25%20thick%204.00%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. AH 79-100 A
3. FX 60-100
4. OAF095
5. Joukowsky 9.00% thick 4.00% camber
6. Joukowsky 11.00% thick 4.00% camber
7. EM J18 3510 26 51
8. FX 60-100 (126)
9. FX 60-100 10.0% smoothed
10. GOE 602 MOD.
11. MH 38 9.68%
12. SD7043 (9.1%)
13. GOE 115 (MVA MK.2)
14. OAF102
15. DAE-51
16. NACA63-610 a=0.8
17. MH 116 9.84%
18. NACA63-710
19. SB99 F3J
20. HOBIE
21. SD7032-099-88