Similarly shaped airfoils to FX S 02/1-158
New! Bulk download of polars in Excel format: fxs21158.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA63(2)-615
3. FX 63-145
4. MID 415
5. NACA63-715
6. FX 61-147
7. NACA63-714
8. MS3,3-15GP
9. DU 80-141
10. HQ 3.5/14
11. Joukowsky 15.00% thick 4.00% camber
12. NACA63-615 a=0.8
13. NACA63-614 a=0.8
14. AH 93-W-145
15. NACA63-615 a=0.6
16. NACA63-614 a=0.6
17. WB-135/35 13.5% smoothed
18. GA 35-415
19. GA 35-414
20. MS3/15GPV
21. NACA63-615 a=0.5