Similarly shaped airfoils to NM Retro 16
New! Bulk download of polars in Excel format: NM%20Retro%2016.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. Joukowsky 16.00% thick 4.00% camber
5. Joukowsky 16.00% thick 5.00% camber
6. GOE 413
7. EPPLER 562
8. Joukowsky 15.00% thick 4.00% camber
9. EPPLER 560
10. Joukowsky 17.00% thick 4.00% camber
11. Joukowsky 17.00% thick 5.00% camber
12. Joukowsky 15.00% thick 5.00% camber
13. GOE 626
14. MID 415
15. MID 403
16. MS535-2
17. NM Retro 14
18. GOE 433
19. GOE 645
20. EPPLER 561
21. GS-1