Similarly shaped airfoils to HG(1)-1715
New! Bulk download of polars in Excel format: HG%281%29-1715.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. FX 73-CL3-152
3. GOE 630
4. EPPLER 422
5. GOE 226 (MVA H.36)
6. FX 74-CL6-140
7. GOE 441
8. JN-153
9. FX 73-CL2-152
10. GOE 366
11. GOE 225 (MVA H.35)
12. GOE 227 (MVA H.37)
13. GOE 482
14. GOE 447
15. Joukowsky 14.00% thick 8.00% camber
16. MH 113 14.62%
17. EPPLER 591
18. GOE 242 (MVA PR.2)
19. GOE 592
20. Joukowsky 13.00% thick 8.00% camber
21. Joukowsky 15.00% thick 8.00% camber