Similarly shaped airfoils to MS535-2
New! Bulk download of polars in Excel format: MS535-2.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. GOE 650
3. USA 40
4. NM Retro 13
5. GS-1
6. GOE 619
7. Joukowsky 14.00% thick 4.00% camber
8. GOE 550
9. Joukowsky 14.00% thick 5.00% camber
10. USA 40 B
11. GOE 685
12. GOE 430
13. EPPLER 562
14. EPPLER 210
15. SD7062 (14%)
16. Joukowsky 15.00% thick 5.00% camber
17. Joukowsky 13.00% thick 4.00% camber
18. Joukowsky 15.00% thick 4.00% camber
19. Joukowsky 13.00% thick 5.00% camber
20. FX 63-145
21. GOE 298