Similarly shaped airfoils to Joukowsky 14.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2014.00%25%20thick%203.00%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 15.00% thick 3.00% camber
3. SB96D TRAINER
4. EM J18 3013
5. EPPLER 203
6. EPPLER 715
7. HN-975TA
8. MS2.5/13GPV
9. SB 96 12.7/3.0
10. MS3/13GPV
11. SB99A22C4
12. NACA63-614
13. HN-956
14. NACA63-514 a=0.8
15. EPPLER 197
16. HN-975
17. DU 80-141
18. Joukowsky 12.00% thick 3.00% camber
19. EM L3 3012
20. Joukowsky 16.00% thick 3.00% camber
21. NACA63-613