Similarly shaped airfoils to JN-153
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. UA(2)-180 smoothed
5. MH 112 16.2%
6. FX 72-LS-160
7. GOE 228 (MVA H.38)
8. GOE 592
9. FX 73-CL3-152
10. MH 113 14.62%
11. GOE 242 (MVA PR.2)
12. FX 74-CL6-140
13. EPPLER 591
14. GOE 572
15. GOE 241 (MVA PR.1)
16. EPPLER 422
17. Joukowsky 17.00% thick 8.00% camber
18. GOE 366
19. Joukowsky 16.00% thick 8.00% camber
20. UA(2)-180
21. FX 72-MS-150A