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Experimental Slender Wing Model Design by the Application of Aeroelastic Scaling Laws
Publisher: American Society of Civil Engineers
Abstract: Long-endurance, unmanned air vehicles (UAVs) usually employ high-aspect-ratio, flexible wings to reduce weight and power required to achieve extended flight operation. There are currently several advanced concept designs ...
Structural Uncertainty Effect on Classical Wing Flutter Characteristics
Publisher: American Society of Civil Engineers
Abstract: Flutter-critical velocity is usually estimated from deterministic analyses by assuming that physical and geometrical parameters are perfectly known. However, aleatory and epistemic uncertainties, especially those associated ...
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