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A feasible method of measuring the aircraft wing deformation based on fiber Bragg grating (FBG) is introduced. The strains of the wing can be obtained by means of FBGs attached on the surface of the model airfoil. A finite element model (FEM) is established to obtain the numerical analysis results of strain and deformation of the wing. The experimental deformation of the airfoil can be deduced by...
A VHF bent monopole antenna mounted on an Army UAV wing platform is modeled and simulated using the FEKO electromagnetic simulation software package and the results are compared with measured radiation pattern data. In order to reduce the complexity of the final FEKO simulation and minimize its runtime and memory usage, the simplification of the composite wing structure as a PEC wing is verified through...
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