Similarly shaped airfoils to MS535-3V
New! Bulk download of polars in Excel format: MS535-3V.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. FX 60-126
3. JWL041 11/3.5
4. Joukowsky 13.00% thick 4.00% camber
5. EM L3 3012
6. FX 60-126/1
7. Joukowsky 11.00% thick 4.00% camber
8. EM J18 3212
9. SB96 11.6/3.0
10. MID 343
11. MS3,3-11GP
12. Joukowsky 12.00% thick 3.00% camber
13. EM J18 3012 DrW r1,2
14. EPPLER 393
15. GOE 546
16. HQ 3.5/12
17. GOE 685
18. K3311 (original)
19. MS3,3-11GPT
20. K3311 (smoothed)
21. SBC3