Detecting barely visible impact damage detection on aircraft composites structures

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Impact damage identification in composite laminates using vibration testing (2014, methodology): “Despite the extensive studies of vibration analysis on damaged laminated composites, the literature reviewed concentrates primarily on Levels 1 and 2 of damage identification Polimeno and Meo [21], Aymerich and Staszewski [22], Ooijevaar et al.”
Acoustic structural health monitoring of composite materials : Damage identification and evaluation in cross ply laminates using acoustic emission and ultrasonics (2012, methodology): “Acoustic methods in their passive (Acoustic Emission, AE) and active (ultrasonic testing, UT) form can provide crucial information for both purposes [3–7].”
Barely visible impact damage assessment in laminated composites using acoustic emission (2018, methodology): “[12] used the Nonlinear Elastic Wave Spectroscopy (NEWS) to detect BVID in carbon fiber composite plates.”
Damage identification in aircraft composite structures: A case study using various non-destructive testing techniques (2015, background): “The danger of such damage is that in most cases they are invisible on the surface and cannot be detected during visual inspections of the structure, hence they are often called Barely Visible Impact Damage (BVID) [1–5].”