Similarly shaped airfoils to MS535-1
New! Bulk download of polars in Excel format: MS535-1.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 559
3. EPPLER 793
4. GOE 413
5. Joukowsky 16.00% thick 5.00% camber
6. Joukowsky 16.00% thick 4.00% camber
7. Joukowsky 17.00% thick 5.00% camber
8. EPPLER 560
9. GOE 626
10. EPPLER 562
11. Joukowsky 15.00% thick 5.00% camber
12. Joukowsky 15.00% thick 4.00% camber
13. Joukowsky 17.00% thick 4.00% camber
14. GOE 645
15. MID 415
16. MID 403
17. GOE 433
18. MS535-2
19. EPPLER 561
20. GOE 648
21. NM Retro 14