The effect of aerofoil shape on rubber powered model aircraft

AI Thread Summary
Aerofoil shape significantly influences the performance of rubber-powered model aircraft, which can successfully fly with various wing designs, including flat, cambered, thick, and thin wings. In manned aircraft, aerofoil shape is crucial for structural integrity and stall behavior, but for rubber-powered models, weight reduction and structural strength are prioritized. The models typically operate with a brief power burst, necessitating a stable flight pattern despite the aerofoil design. The discussion highlights the trade-off between minimizing weight and maximizing lift-to-drag ratio (L/D) while maintaining adequate strength. Understanding these dynamics is essential for optimizing performance in small rubber-powered aircraft.
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Model aircraft display a wide range of aerofoil shapes, and many of these models fly despite the shape of the cross section of the wing.

Models with flat wings, cambered wings, thick wings, thin wings - all of these fly succesfully.

What is the function of aerofoil shape on free flight rubber powered models - between 30 to 60 cm in span? In manned aircraft, the aerofile shape is said to depend on required structural thickness, and stall behaviour, that is, a gentler stall rather than a sharp one where lift suddenly reduces.

Specifically in model aircraft of the rubber powered free flight variety, it seems more important to make an effort to reduce weight and thickness, however I am not sure what the effect on performance might be, given that these models run with a short burst of ever decreasing power, and should fly a stable flight pattern.
 
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It's just a trade-off between reducing weight, attaining sufficient structural strength, and getting the best L/D under those constraints.
 
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