Similarly shaped airfoils to NM Retro 14


New! Bulk download of polars in Excel format: NM%20Retro%2014.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
Dynamic plotter New!
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.

1. MS535-2
2. GOE 650
3. NM Retro 13
4. USA 40
5. Joukowsky 14.00% thick 4.00% camber
6. Joukowsky 14.00% thick 5.00% camber
7. GOE 550
8. GS-1
9. EPPLER 562
10. GOE 430
11. GOE 619
12. EPPLER 210
13. USA 40 B
14. GOE 685
15. Joukowsky 13.00% thick 4.00% camber
16. Joukowsky 15.00% thick 5.00% camber
17. FX 63-145
18. Joukowsky 15.00% thick 4.00% camber
19. Joukowsky 13.00% thick 5.00% camber
20. SD7062 (14%)
21. FX 60-126/1