Similarly shaped airfoils to JN-153
New! Bulk download of polars in Excel format: jn153.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 482
3. EPPLER 421
4. HG(1)-1715
5. UA(2)-180 smoothed
6. MH 112 16.2%
7. FX 72-LS-160
8. GOE 228 (MVA H.38)
9. GOE 592
10. FX 73-CL3-152
11. MH 113 14.62%
12. GOE 242 (MVA PR.2)
13. FX 74-CL6-140
14. EPPLER 591
15. GOE 572
16. GOE 241 (MVA PR.1)
17. EPPLER 422
18. Joukowsky 17.00% thick 8.00% camber
19. GOE 366
20. Joukowsky 16.00% thick 8.00% camber
21. UA(2)-180