Similarly shaped airfoils to FX 74_CL5_140
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 440
3. EPPLER 423
4. EPPLER 420
5. FX 72-MS-150B
6. CH10 (smoothed)
7. GOE 448
8. Joukowsky 13.00% thick 10.00% camber
9. Joukowsky 14.00% thick 10.00% camber
10. GOE 523
11. GOE 525
12. GOE 482
13. Joukowsky 12.00% thick 10.00% camber
14. Joukowsky 15.00% thick 10.00% camber
15. S1223 RTL
16. EPPLER 421
17. FX 72-MS-150A
18. Joukowsky 13.00% thick 9.00% camber
19. Joukowsky 11.00% thick 10.00% camber
20. Joukowsky 14.00% thick 9.00% camber
21. Joukowsky 16.00% thick 10.00% camber