Similarly shaped airfoils to St. CYR 172 (Royer)
New! Bulk download of polars in Excel format: stcyr172.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 474
3. Horten 14.00% thick 0.00% camber
4. Horten 13.00% thick 0.00% camber
5. NACA0013
6. GA 30A013
7. GA 30-013
8. GA 30-014
9. GA 30A014
10. GOE 459
11. EPPLER 169
12. RAF 30
13. FX LIII-142 K 25
14. Horten 14.00% thick 1.00% camber
15. HM50T
16. GOE 409
17. Horten 13.00% thick 1.00% camber
18. FX 76-120
19. Joukowsky 14.00% thick 0.00% camber
20. FX 71-120
21. GA 35-014