Similarly shaped airfoils to GU25-5(11)8
New! Bulk download of polars in Excel format: gu255118.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (6) | 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. DRAGONFLY CANARD
3. RONCZ 1046 VOYAGER CANARD
4. GOE 798
5. GOE 625
6. GOE 390
7. GOE 382
8. GOE 422
9. USA 34
10. GOE 518
11. GOE 614
12. USA 35
13. USA 35 A
14. UA(2)-180
15. GOE 514
16. GOE 421
17. UA(2)-180 smoothed
18. FX 73-170 A
19. GOE 620
20. GOE 504
21. GOE 449