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Showing 1 to 3 of 3 for “"Smart Wing"”.
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Develpoment of advanced structural multifield models for the study of smart wing
… control the behaviour of an distributed actuated wing are necessary model with low computational times. In fact the computational time must be lower than the characteristic time of the controlled phenomenon. In this contest it is very interesting try to identify a method able to build reduced …
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Dynamic Modeling of a Supersonic Tailless Aircraft with All-moving Wingtip Control Effectors
… with determining the necessary rolling and yawing moment coefficients necessary to meet the rest of the chosen dynamic response requirements. These coefficients were then used to find the corresponding all-moving tip deflections. The CFD data showed that even at small all-moving tip …
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Characterization of Oscillatory Lift in MFC Airfoils
The purpose of this research is to characterize the response of an airfoil with an oscillatory morphing, Macro-fiber composite (MFC) trailing edge. Correlation of the airfoil lift with the oscillatory input is presented. Modal analysis of the test airfoil and apparatus is used to determine the …