Similarly shaped airfoils to WACO COOTIE
New! Bulk download of polars in Excel format: cootie.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. GOE 336 (MVA H.44)
3. GOE 287
4. GOE 326 (PFALZ 55)
5. GOE 610 B
6. GOE 199 (L.F.G. 5406)
7. USA 25
8. GOE 140 (MVA H.17)
9. GOE 281 (DAIMLER XII)
10. GOE 310 (MVA H.42)
11. NACA64-709 a=0.5
12. GOE 325 (PFALZ 54)
13. GOE 280 (DAIMLER XI)
14. NACA63-709 a=0.5
15. GOE 274 (DAIMLER V)
16. NACA65-709 a=0.5
17. GOE 184 (MVA H.29)
18. GOE 314 (HANSA-BRANDENBURG)
19. GOE 407
20. GOE 277 (DAIMLER VIII)
21. GOE 311 (MVA H.43)