Similarly shaped airfoils to USA 98
New! Bulk download of polars in Excel format: usa98.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. Joukowsky 14.00% thick 7.00% camber
3. Joukowsky 16.00% thick 7.00% camber
4. GOE 502
5. GOE 501
6. MH 114 13.02%
7. EPPLER 591
8. Joukowsky 15.00% thick 6.00% camber
9. FX 63-137
10. Joukowsky 14.00% thick 6.00% camber
11. Joukowsky 13.00% thick 7.00% camber
12. FX 73-CL2-152
13. FX 63-137 13.7% smoothed
14. MH 113 14.62%
15. GOE 446
16. Joukowsky 16.00% thick 6.00% camber
17. MID 406w2
18. FX 76-MP-140
19. Joukowsky 17.00% thick 7.00% camber
20. GOE 535
21. Joukowsky 13.00% thick 6.00% camber