Similarly shaped airfoils to GOE 188
New! Bulk download of polars in Excel format: goe188.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 280 (DAIMLER XI)
3. GOE 134 (MVA H.12)
4. GOE 287
5. GOE 257
6. GOE 180 (MVA H.26)
7. GOE 167 (V.KARMAN PROP.2)
8. GOE 328
9. GOE 281 (DAIMLER XII)
10. AQUILA 9.3% smoothed
11. GOE 316 (HANSA-BRANDENBURG IV.5)
12. NACA64-709 a=0.2
13. NACA65-709 a=0.2
14. GOE 286
15. GOE 326 (PFALZ 55)
16. GOE 385
17. GOE 325 (PFALZ 54)
18. NACA63-709 a=0.2
19. GOE 314 (HANSA-BRANDENBURG)
20. GOE 309 (MVA H.41)
21. GOE 308 (MVA H.40)