Similarly shaped airfoils to Joukowsky 15.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2015.00%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 16.00% thick 3.00% camber
3. MID 393 UL
4. EPPLER 715
5. MID 327 15%
6. S2027
7. MS2.5/15GPV
8. GOE 629
9. Joukowsky 13.00% thick 3.00% camber
10. Joukowsky 17.00% thick 3.00% camber
11. Joukowsky 15.00% thick 4.00% camber
12. Joukowsky 15.00% thick 2.00% camber
13. NACA63-615
14. NACA63-515 a=0.8
15. MS3/15GPV
16. EM J18 2515 DrW r0,8
17. EM J18 1 3015
18. NACA63-614
19. NACA63-514 a=0.8
20. EPPLER 203
21. NACA63-515