Similarly shaped airfoils to AH 94-145
New! Bulk download of polars in Excel format: ah94145.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. GOE 414
3. AH 95-160
4. GOE 412
5. MID 321e
6. GOE 387
7. GOE 476
8. FX 67-K-150/17
9. NACA65-715 a=0.6
10. NACA65-714 a=0.6
11. GOE 398
12. MID 393
13. NACA64-715 a=0.6
14. GOE 612
15. GOE 621
16. GOE 615
17. NACA65-715 a=0.5
18. NACA65-714 a=0.5
19. NACA63-715 a=0.6
20. DOUGLAS LA203A
21. NACA64-714 a=0.6