Polymer Composites in the Aerospace Industry 2020
DOI: 10.1016/b978-0-08-102679-3.00018-6
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Lightning strike direct effects

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Cited by 3 publications
(4 citation statements)
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“…A high factor of a power outage due to lightning has also been reported in some countries [1]. Despite recent progress in the area of overvoltage protection, current statistical data that has been used around the world show that lightning activity remains the dominant factor affecting the overhead failure rate [2][3][4][5][6]. Analyzing the basic causes of failures in power networks based on the data presented in Fig.…”
Section: Introductionmentioning
confidence: 99%
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“…A high factor of a power outage due to lightning has also been reported in some countries [1]. Despite recent progress in the area of overvoltage protection, current statistical data that has been used around the world show that lightning activity remains the dominant factor affecting the overhead failure rate [2][3][4][5][6]. Analyzing the basic causes of failures in power networks based on the data presented in Fig.…”
Section: Introductionmentioning
confidence: 99%
“…The failure rate of the other elements is about the same. The analyses can be divided into several categories: theoretical studies based on simplified analytical formulas [3,5,9,10], computer simulations based on the finite element method [11][12][13][14]. The results of the analysis of some models indicate that the impact on the level of overvoltages has wire location and grounding parameters [15][16][17].…”
Section: Introductionmentioning
confidence: 99%
“…Simulation literature has therefore interpreted the real physical test conditions appropriate for the simulation type. In a realistic strike scenario, lightning current will have a point of entry and a remote point of exit [31]. This creates specific local conditions in which current will flow predominantly in the direction of the exit via the path of least resistance [31].…”
mentioning
confidence: 99%
“…In a realistic strike scenario, lightning current will have a point of entry and a remote point of exit [31]. This creates specific local conditions in which current will flow predominantly in the direction of the exit via the path of least resistance [31]. Thus, specimen experimental boundary conditions in a laboratory (where specimens are typically <1 m in length) do not necessarily represent those in a real aircraft (where panels can be >1 m in length).…”
mentioning
confidence: 99%