In an article published in the journal Aerospace, researchers achieved realtime monitoring of strains and structural displacements for the target Joined-Wing aircraft via Fiber Optic Sensing System (FOSS). The Joined-Wing layout is often seen to provide a significant gain in design space and offer additional alternatives in propulsion, aeroelasticity, flight dynamics, aeroelasticity aerodynamics, and other areas. Real-time structural deformation measurement is crucial in structural health monitoring (SHM), methodology validation, safety evaluation, and structural control.
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