Similarly shaped airfoils to HL73-650
New! Bulk download of polars in Excel format: HL73-650.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. Eiffel 36
3. GOE 195
4. Joukowsky 9.00% thick 6.00% camber
5. Joukowsky 9.00% thick 5.00% camber
6. GOE 495
7. GOE 499
8. GOE 456
9. GOE 458
10. NACA63-709 a=0.8
11. GOE 484
12. NACA64-709 a=0.8
13. EPPLER 471
14. NACA5509
15. MID 117
16. GOE 610-B MOD.
17. AH-6-40-7
18. MID 151b
19. Joukowsky 10.00% thick 6.00% camber
20. GOE 118 (MVA MK.7)
21. NACA6409