Similarly shaped airfoils to Joukowsky 13.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2013.00%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 14.00% thick 3.00% camber
3. EM L3 3012
4. HN-975TA
5. SB 96 12.7/3.0
6. NM RETRO tip for 30% ailerons
7. HN-975
8. SB96D TRAINER
9. NM RETRO tip for 50% ailerons
10. HN-974
11. EM J18 3013
12. MID 327 12%
13. NM32 root
14. EPPLER 201
15. HN-475
16. EM J18 3012 DrW r1,2
17. MS2.5/13GPV
18. FX 60-126
19. HN-959
20. HN-832TA
21. PT40 (Great Planes Trainer)