Which is the airfoil having highest lift to drag ratio?

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Discussion Overview

The discussion centers around identifying airfoils with the highest lift-to-drag ratio, particularly in the context of a new airfoil design. Participants explore various airfoil series, their applications, and design considerations, including hybrid and morphing wings.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested
  • Homework-related

Main Points Raised

  • One participant requests information on the airfoil with the highest lift-to-drag ratio for comparison purposes.
  • Another participant notes the vast number of airfoil designs and suggests that the original poster (OP) could conduct research to find this information.
  • A participant suggests that knowing the series of airfoils would be helpful.
  • There is a request for coordinate files of wings used in sailplanes or laminar flow wings, indicating a need for specific design data.
  • One participant mentions that morphing wings are currently a significant area of research among hybrid wing designs.
  • The OP reiterates their request for airfoils with high lift-to-drag ratios and mentions NACA aerofoils, specifically the NACA 64A309 Hydrofoil, and recommends using XFLR5 software for analysis.
  • Another participant highlights the Selig 1223 and Epler 423 airfoils as commonly used in aerodesign competitions due to their favorable lift-to-drag ratios.
  • A participant proposes that a blended wing body design, like that of the B-2, could achieve high lift but notes the complexity of controlling such designs.
  • There is a caution regarding the control challenges associated with blended wing body designs, emphasizing the need for advanced control systems.
  • Another participant suggests researching airfoils used by high-performance gliders for further insights.

Areas of Agreement / Disagreement

Participants express various viewpoints on airfoil designs and their performance characteristics, with no consensus on a single airfoil or design approach being established. Multiple competing views and suggestions remain present throughout the discussion.

Contextual Notes

Participants reference specific airfoil series and designs without providing detailed comparisons or empirical data. The discussion lacks definitive conclusions regarding the best airfoil for lift-to-drag ratio, and assumptions about design effectiveness and control complexities are present.

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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