Which is the airfoil having highest lift to drag ratio?

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SUMMARY

The airfoils with the highest lift-to-drag ratios include the NACA 64A309 Hydrofoil, Selig 1223, and Epler 423, which are commonly utilized in aerodesign competitions. For advanced designs, blending fuselage with wings, as seen in the B-2, enhances aerodynamic efficiency. Tools like XFLR5 software are recommended for analyzing various NACA aerofoils. Additionally, morphing wings represent a significant area of research in modern aerodynamics.

PREREQUISITES
  • Understanding of NACA aerofoil series
  • Familiarity with aerodynamic principles
  • Experience using XFLR5 software for airfoil analysis
  • Knowledge of blended wing body design concepts
NEXT STEPS
  • Research the NACA 64A309 Hydrofoil specifications
  • Analyze the performance of Selig 1223 and Epler 423 airfoils
  • Explore advanced aerodynamic design principles for blended wing bodies
  • Learn about morphing wing technologies and their applications
USEFUL FOR

Aerospace engineers, aerodynamics researchers, and students involved in airfoil design and optimization will benefit from this discussion.

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..
 
Last edited:
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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