Similarly shaped airfoils to FX 73-170 A
New! Bulk download of polars in Excel format: fx73170a.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. AH 95-160
3. EPPLER 654
4. EPPLER 656
5. GOE 449
6. GOE 423
7. EPPLER 657
8. GOE 692
9. NACA65-717 a=0.6
10. GOE 508
11. FX 73-K-170/22
12. GOE 504
13. GOE 797
14. RONCZ 1046 VOYAGER CANARD
15. NACA66-716 a=0.6
16. FX 08-S-176
17. GOE 506
18. NACA65-717 a=0.5
19. NACA66-717 a=0.6
20. GA 40A617
21. NACA65-718 a=0.6