Similarly shaped airfoils to NLR-1T
New! Bulk download of polars in Excel format: nlr1t.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
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2. MH 24 9.01%
3. SIKORSKY SSC-A09
4. MH 34
5. GIII BL332
6. ONERA OA209
7. MH 23 8%
8. BOEING 737 MIDSPAN
9. TsAGI B 9.0% thick
10. GIII BL288
11. NACA67-209 a=0.2
12. NACA66-209 a=0.2
13. GIII BL369
14. NACA67-209 a=0.5
15. GIII BL126
16. NACA67-209 a=0.0
17. EPPLER 904
18. NACA66-209 a=0.5
19. NACA66-209 a=0.0
20. TsAGI B 9.5% thick
21. NACA67-209 a=0.6