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en línea
Lance W. Traub    
An investigation of the lift components present over low aspect ratio rectangular wings is presented. Wing aspect ratios ranging from 0.5 to 3 are examined using published experimental results and analytic analysis methods. The methods are based on the f... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lance W. Traub and Mashaan P. Kaula    
One of the most commonly implemented devices for stall control on wings and airfoils is a leading-edge slat. While functioning of slats at high Reynolds number is well documented, this is not the case at the low Reynolds numbers common for small unmanned... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lance W. Traub    
A semi-empirical method is presented to estimate the angular excursion and the lift loss associated with static hysteresis on an airfoil. Wind tunnel data of various airfoils is used to define and validate the methodology. The resulting equation provides... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Lance W. Traub    
Revista: Batteries    Formato: Electrónico

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