Similarly shaped airfoils to LNV109A
New! Bulk download of polars in Excel format: lnv109a.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. MH 84 13.69%
3. UI-1720
4. GOE 323 (HANSA-BRANDENBURG V.1)
5. EPPLER 593
6. GOE 769
7. EPPLER 598
8. GOE 534
9. GOE 324 (HANSA-BRANDENBURG)
10. MILEY M06-13-128
11. GOE 238 (HANSA-BRANDENBURG)
12. GOE 532
13. GOE 321 (HANSA-BRANDENBURG III.1)
14. MUE 139
15. GOE 319 (HANSA-BRANDENBURG II)
16. GOE 418
17. LISSAMAN 7769
18. FX 77-W-121
19. S4180-098-84
20. GOE 746
21. FX 73-CL1-152