Feasibility and Advantages of Variable Wing Area Concept in UAV/RC Aircraft

AI Thread Summary
The discussion centers on a final year aeronautical engineering project exploring the feasibility of a variable wing area concept in UAVs/RC aircraft. The proposed method involves adjusting wing area asymmetrically to induce roll and using flaperons for controlled dives, mimicking eagle flight behavior. Participants are prompted to consider the advantages of this approach compared to traditional spoilers. The feasibility of the concept is questioned, with requests for insights based on existing research and findings. The conversation emphasizes the need for thorough investigation into aerodynamic principles and practical applications.
devilidol
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Hey guys!,
this is my final year aeronautical engineering project that me and my group are going to work on!
we have this concept of producing a roll in an uav/RC aircraft by reducing the area of the wing on one side while keeping the other side area constant or increasing it(gradually)
and using the flaperon setting to reduce the area equally on both sides for a dive basically how a eagle would do
so my question is, is this feasible if yes, what do you guys think would be the advantages over spoilers?
if no, why?

thanks!
 
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devilidol said:
Hey guys!,
this is my final year aeronautical engineering project that me and my group are going to work on!
we have this concept of producing a roll in an uav/RC aircraft by reducing the area of the wing on one side while keeping the other side area constant or increasing it(gradually)
and using the flaperon setting to reduce the area equally on both sides for a dive basically how a eagle would do
so my question is, is this feasible if yes, what do you guys think would be the advantages over spoilers?
if no, why?

thanks!

Welcome to the PF.

Since this is a schoolwork question, please share what you have found so far in your reading and research... :smile:
 

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