Similarly shaped airfoils to EPPLER 396
New! Bulk download of polars in Excel format: e396.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. EPPLER 395
3. RAF 32
4. GOE 497
5. GOE 567
6. FX 63-137 13.7% smoothed
7. GOE 430
8. EPPLER 399
9. Joukowsky 14.00% thick 6.00% camber
10. Joukowsky 13.00% thick 6.00% camber
11. Joukowsky 13.00% thick 5.00% camber
12. Joukowsky 14.00% thick 5.00% camber
13. FX 63-120
14. GOE 414
15. GOE 412
16. Joukowsky 15.00% thick 6.00% camber
17. GOE 501
18. GOE 480
19. FX 63-137
20. NACA63-713 a=0.8
21. Joukowsky 12.00% thick 6.00% camber