Which is the airfoil having highest lift to drag ratio?

AI Thread Summary
The discussion centers on identifying airfoils with the highest lift-to-drag ratios for a new design project. Participants emphasize the vast number of airfoil designs available, suggesting that researching specific series, such as NACA aerofoils, could be beneficial. Notable high lift airfoils mentioned include the Selig 1223 and Epler 423, which are favored in aerodesign competitions. The conversation also touches on advanced concepts like blended wing body designs, highlighting their aerodynamic advantages and the need for sophisticated control systems. Overall, the thread provides insights into airfoil selection and design considerations for optimal performance.
sr241
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I working on a new airfoil design. Please tell me the airfoil having highest lift to drag ratio, I need it for comparison.
 
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You realize there are hundreds and hundreds of airfoil designs, right?

I doubt anyone knows that off the top of their head, and you can research it as easily as any of us.
 
if you could tell me at least which series then it will be very helpful
 
where can i get coordinate files of wings of sail planes or coordinate files of laminar flow wings. please tell me the names of these wings
 
There occurs various hybrid wings; however currently the most researched is Morphing Wings
 
sr241 said:
I working on a new airfoil design. Please tell me the airfoil having highest lift to drag ratio, I need it for comparison.

Search NACA aerofoils one of them is NACA 64A309 Hydrofoils,try analysing different NACA aerofoils in XFLR5 software, its free easy to use..
 
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thanks
 
high lift airfoils that are commonly used in aerodesign competition is the Selig 1223 and Epler 423, due to the great lift to drag ratio...
 
  • #10
Good luck controlling a blended wing body design though. You need sophisticated, computerized control systems to successfully keep such designs airborne and stable.
 
  • #11
OP, research the airfoils used by high performance gliders...
 
  • #12
boneh3ad said:
Good luck controlling a blended wing body design though. You need sophisticated, computerized control systems to successfully keep such designs airborne and stable.


you got that right:)
 
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