Research Article
An Analytical-Based Lightning-Induced Damage Model for an Aircraft Wing Exposed to Pressure Loading of Lightning
Table 8
Comparison of the magnitudes of the pressure models for 200 kA lightning current.
| | Magnitude of the electromagnetic pressure impact of lightning | | Time () | For 200 kA lightning current | | IEPIM (Pa) | EMMA [57] (Pa) | Relative error (%) | SDICOM [57] (Pa) | Relative error (%) |
| | t = 6 | | | 3.6 | | 7.6 | | t = 9 | | | 12.7 | | 0.6 | | t = 14 | | | 20.1 | | 8.6 | | t = 26 | | | 4.8 | | 0.9 |
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