Abstract Recently, Non-destructive Ultrasonic Techniques have been utilized to detect aircraft icing. Traditional methods like ultrasound pulse-echo, guided waves, and optics are unsuitable due to ice’s complex properties and shape. Pulse-echo ultrasound, reliant on surface layer travel time, becomes ineffective with thin ice layers and variable ice properties. This research aimed to reconstruct ice properties and geometry on aircraft surfaces using ultrasonic full waveform inversion (FWI). For simulation COMSOL software is used to verify wave propagation through a nonlinear, thinly layered model. Wave propagation is then modelled using the 2D acoustic equation and finite differential methods, generating synthetic data. The FWI algorithm implemented, utilizes this synthetic data to reconstruct material properties and ice shape. Crucially, ultrasound transducers are discreetly positioned beneath the aircraft skin to non-destructively gather ice information without affecting aerodynamics.
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