1996
DOI: 10.1117/12.239026
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<title>High-frequency impedance analysis for NDE of complex precision parts</title>

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Cited by 30 publications
(18 citation statements)
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“…The natural frequency ofthe beam in bending mode has well-known solution for the first several modes, which is fr/ (5) 2ic pA where IT 5 the natural frequency of the bending mode, 3,. is the weighted frequency for the each mode and I , A are the area moment of inertia and area of the cross section, respectively, of the beam. This equation can be rewritten to account for the temperature dependency ofthe material properties by incorporating equations (2-4) as follows:…”
Section: Variation In Structural Dynamic Characteristics Caused By Chmentioning
confidence: 99%
“…The natural frequency ofthe beam in bending mode has well-known solution for the first several modes, which is fr/ (5) 2ic pA where IT 5 the natural frequency of the bending mode, 3,. is the weighted frequency for the each mode and I , A are the area moment of inertia and area of the cross section, respectively, of the beam. This equation can be rewritten to account for the temperature dependency ofthe material properties by incorporating equations (2-4) as follows:…”
Section: Variation In Structural Dynamic Characteristics Caused By Chmentioning
confidence: 99%
“…Experimental implementation of the impedance-based structural health monitoring technique has been successfully conducted on several complex structures: a four bay space truss (Sun et al 1995), an aircraft structure , complex precision parts (Lalande et al 1996), temperature varying applications (Park et al1999), a spotwelded structural joints (Giurgiutiu et al 1999), civil structural components (Park et al, 2000), a reinforced concrete bridge (Soh et al 2000) and civil pipelines (Park et al 2001a). …”
Section: Structurementioning
confidence: 99%
“…Experimental i mplementation of the piezoimpedance method has been successfully conducted on several complex structures; a quarter model of steel girder bridge [3], a composite reinforced concrete wall [3], a massive cylinder header [4], a high precision gear [5], a space structure [5] and an aircraft [6]. For above real structures, a spring-mass model as shown in Fig.2 has been adopted.…”
Section: Previous Studies and Problemsmentioning
confidence: 99%