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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 ...
Engineering Method for Air-Cooling Design of Two-Seat Propeller-Driven Aircraft Powered by Fuel Cells
Publisher: American Society of Civil Engineers
Abstract: The application of fuel-cell technology to aircraft propulsion and/or energy supply is becoming of great interest for undoubted advantages in terms of pollution emissions and noise, features particularly important for ...
Air Cooling of a Two-Seater Fuel Cell–Powered Aircraft: Dynamic Modeling and Comparison with Experimental Data
Publisher: American Society of Civil Engineers
Abstract: The application of fuel cell (FC) technology to aircraft propulsion and/or energy supply is becoming of great interest for undoubted advantages in terms of pollution emissions and noise reduction. A better understanding ...
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