Similarly shaped airfoils to FX 73-CL1-152
New! Bulk download of polars in Excel format: fx73cl1152.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 534
3. GOE 535
4. GOE 654
5. GOE 615
6. EPPLER 422
7. MID 393
8. GOE 322 (HANSA-BRANDENBURG IV.1)
9. GOE 528
10. GOE 324 (HANSA-BRANDENBURG)
11. GOE 553
12. GOE 533
13. GOE 418
14. MH 84 13.69%
15. GOE 387
16. GOE 320 (HANSA-BRANDENBURG II.1)
17. GOE 645
18. GOE 404
19. Joukowsky 14.00% thick 6.00% camber
20. Joukowsky 15.00% thick 6.00% camber
21. MH 83 13.29%